Calculators Created by Anshika Arya

Created Crippling Load for any type of End Condition

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Created Crippling Load given Effective Length and Radius of Gyration

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Created Crippling Stress

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Created Crippling Stress given Crippling Load

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Created Eccentric Point Load for Fixed Beam

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Created Eccentric Point Load for Simply Supported Beam

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Created Value of Load for Cantilever Beam with Point Load at Free End

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Created Value of Load for Cantilever Beam with Uniformly Distributed Load

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Created Value of Load for Fixed Beam with Central Point Load

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Created Value of Load for Fixed Beam with Uniformly Distributed Load

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Created Value of Load for Simply Supported Beam with Central Point Load

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Created Value of Load for Simply Supported Beam with Uniformly Distributed Load

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Verified Front Lateral Load Transfer given Load on Front Inside Wheel in Cornering

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Verified Front Lateral Load Transfer given Load on Front Outside Wheel in Cornering

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Verified Rear Lateral Load Transfer given Load on Rear Inside Wheel in Cornering

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Verified Rear Lateral Load Transfer given Load on Rear Outside Wheel in Cornering

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Verified Wheel Load on Front Inside Wheel during Cornering

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Verified Wheel Load on Front Inside Wheel in Static Condition given Load during Cornering

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Verified Wheel Load on Front Outside Wheel during Cornering

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Verified Wheel Load on Front Outside Wheel in Static Condition given Load during Cornering

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Verified Wheel Load on Rear Inside Wheel during Cornering

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Verified Wheel Load on Rear Inside Wheel in Static Condition given Load during Cornering

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Verified Wheel Load on Rear Outside Wheel during Cornering

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Verified Wheel Load on Rear Outside Wheel in Static Condition given Load during Cornering

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1 More Load on Wheels in Race Cars Calculators

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Verified Doublet Strength for 3D Incompressible Flow

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Verified Radial Coordinate for 3D Doublet Flow given Velocity Potential

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Verified Radial Coordinate for 3D Source Flow given Radial Velocity

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Verified Radial Coordinate for 3D Source Flow given Velocity Potential

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Verified Radial Velocity for 3D Incompressible Source Flow

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Verified Source Strength for 3D Incompressible Source Flow given Radial Velocity

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Verified Source Strength for 3D Incompressible Source Flow given Velocity Potential

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Verified Velocity Potential for 3D Incompressible Doublet Flow

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Verified Velocity Potential for 3D Incompressible Source Flow

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Verified Absolute velocity for dynamic thrust exerted by jet on plate

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Verified Absolute Velocity for given Normal Thrust Normal to Direction of Jet

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Verified Absolute Velocity for given Normal Thrust Parallel to Direction of Jet

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1 More Absolute velocity Calculators

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Verified AC Potentiometer Phase Angle

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8 More AC Circuits Calculators

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Created Acceleration of Follower after Time t for Cycloidal Motion

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Created Acceleration of Follower for Circular Arc Cam if there's Contact on Circular Flank

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Created Acceleration of Follower for Roller Follower Tangent Cam, there's Contact with Straight Flanks

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Created Acceleration of Follower of Roller Follower Tangent Cam, there's Contact with Nose

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Created Centripetal Acceleration of Point P on Circumference

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Created Centripetal Acceleration of Point P on Circumference when Follower Moves with SHM

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Created Minimum Acceleration of Follower for Circular Arc Cam Contacting with Circular Flank

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Created Minimum Acceleration of Follower for Tangent Cam with Roller Follower

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Verified Torque Required in Lifting Load with Acme Threaded Power Screw

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17 More Acme Thread Calculators

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Verified Addendum Circle Diameter of Large Size Gear

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4 More Addendum Circle Diameter Calculators

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Created Induced drag given span efficiency factor

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Verified Lateral plane span given aspect ratio

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20 More Aerodynamic Drag and its Reduction Calculators

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Verified Tip Speed Ratio with Blade Number

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5 More Aircraft Endurance Calculators

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Verified Crew Weight given Fuel and Empty Weight Fraction

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Verified Crew Weight given Takeoff Weight

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Verified Empty Weight given Empty Weight Fraction

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Verified Empty Weight given Takeoff Weight

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Verified Fuel Fraction given Takeoff Weight and Empty Weight Fraction

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Verified Fuel Weight given Fuel Fraction

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Verified Fuel Weight given Takeoff Weight

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Verified Optimum Range for Jet Aircraft in Cruising Phase

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Verified Optimum Range for Prop-Driven Aircraft in Cruising Phase

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Verified Payload Weight given Fuel and Empty Weight Fractions

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Verified Payload Weight given Takeoff Weight

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Verified Preliminary Endurance for Jet Aircraft

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Verified Preliminary Take Off Weight Built-up for Manned Aircraft

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Verified Preliminary Take off Weight Built-Up for Manned Aircraft given Fuel and Empty Weight Fraction

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Verified Takeoff Weight given Empty Weight Fraction

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Verified Takeoff Weight given Fuel Fraction

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Verified Winglet Friction Coefficient

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5 More Aircraft Preliminary Weight Built Up Calculators

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Verified Air Standard Efficiency for Diesel Engines

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Verified Air Standard Efficiency for Petrol engines

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Verified Air Standard Efficiency given Relative Efficiency

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Verified Mean Effective Pressure in Diesel Cycle

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Verified Work Output for Diesel Cycle

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Verified Work Output for Dual Cycle

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Verified Work Output for Otto Cycle

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4 More Air-Standard Cycles Calculators

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Created Allowable crushing stress of rivet material given crushing strength for double rivet

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Created Allowable crushing stress of rivet material given crushing strength for 'n' number of rivets

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Created Allowable crushing stress of rivet material given crushing strength for single rivet

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Created Allowable crushing stress of rivet material given crushing strength for triple rivet

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Created Allowable shear stress of rivet material given shearing strength if rivet is in double shear

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Created Allowable shear stress of rivet material given shearing strength if rivet is in single shear

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Created Allowable tensile stress in plate given strength of solid plate per pitch length

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Created Allowable tensile stress in plate given tearing strength of rivet

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Created Allowable tensile stress in plates given efficiency of riveted joint

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Verified Phase Shifted Voltage Gain using Transconductance

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Verified Voltage Gain using Single Component of Drain Voltage

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4 More Amplification Factor/Gain Calculators

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Verified Common Mode Gain of BJT

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Verified Total Power Dissipated in BJT

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Verified Total Power Supplied in BJT

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Verified Voltage Gain given Transconductance and Collector Resistance

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12 More Amplification Factor/Gain Calculators

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Verified Input Voltage of Amplifier

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Verified Load Resistance with respect to Transconductance

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Verified Output Voltage Gain given Transconductance

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Verified Output Voltage of Amplifier

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Verified Peak Voltage at Maximum Power Dissipation

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16 More Amplifier Characteristics Calculators

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Verified Longitudinal Strain using Poisson's Ratio

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1 More Analysis of Bar Calculators

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Verified Area of lower end of bar

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Verified Area of upper end of bar

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Created Allowable Tensile Stress given Load Carried by Single Fillet Lap Weld

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Created Allowable Tensile Stress given Total Load Carried by Plates in Compound Weld

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Created Length of Parallel Fillet Weld given Load Carried by Parallel Fillet Weld

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Created Length of Parallel Fillet Weld given Total Load Carried by Plates in Compound Weld

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Created Length of Single Fillet Lap Weld given Load Carried by Single Fillet Lap Weld

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Created Length of Single Fillet Lap Weld given Total Load Carried by Plates in Compound Weld

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Created Load Carried by Parallel Fillet Weld

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Created Load Carried by Single Fillet Lap Weld

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Created Maximum Shear Stress given Load Carried by Parallel Fillet Weld

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Created Maximum Shear Stress given Total Load Carried by Plates in Compound Weld

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Created Thickness of Plates given Load Carried by Parallel Fillet Weld

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Created Thickness of Plates given Load Carried by Single Fillet Lap Weld

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Created Thickness of Plates given Total Load Carried by Plates in Compound Weld

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Created Total Load Carried by Plates in Compound Weld

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Verified Maximum Principal Stress

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Verified Minimum Principal Stress

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Verified Shear Stress on Inclined Plane

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Verified Stress on Inclined Plane

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2 More Analysis of Stresses Calculators

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Created Area of Unsymmetrical Weld

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Created Area of Unsymmetrical Weld given Throat Thickness

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Created Area of Weld given Axial Load on Weld

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Created Axial Load on Angle

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Created Axial Load on Angle given Resistance of Bottom and Top Weld

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Created Axial Load on Weld

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Created Axial Load on Weld given Shear Stress

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Created Shear Stress given Axial Load on Weld

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Created Shear Stress given Axial Load on Welded Connection

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Created Thickness of Plate given Area of Unsymmetrical Weld

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Created Thickness of Plate given Axial Load on Weld

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Created Throat Thickness given Area of Unsymmetrical Weld

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Created Total Length of Weld given Area of Unsymmetrical Weld

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Created Total Length of Weld given Length of Bottom Weld

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Created Total Length of Weld given Length of Top and Bottom Weld

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Created Total Length of Weld given Length of Top Weld

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Created Total Length of Weld given Resistance of Bottom Weld

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Created Total Length of Weld given Resistance of Top Weld

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Created Total Resistance given Resistance of Bottom Weld

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Created Total Resistance given Resistance of Top Weld

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Verified Angle of Inside Lock given Turning Radius of Inner Front Wheel

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Verified Angle of Inside Lock given Turning Radius of Inner Rear Wheel

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Verified Angle of Outside Lock given Turning Radius of Outer Front Wheel

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Verified Angle of Outside Lock given Turning Radius of Outer Rear Wheel

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2 More Angles Acting on Steering System and Axles Calculators

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Verified Caster Angle

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5 More Angles Related to Steering System Calculators

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Verified Axial Load for Back to Back Bearings when Fa by Fr is greater than 1.14

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Verified Axial Load for Back to Back Bearings when Fa by Fr is less than or equal to 1.14

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Verified Axial Load for Singly Mounted Bearings when Fa by Fr is greater than 1.14

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Verified Equivalent Dynamic Load for Back to Back Bearings when Fa by Fr is greater than 1.14

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Verified Equivalent Dynamic Load for Back to Back Bearings when Fa by Fr is less than or equal to 1.14

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Verified Equivalent Dynamic Load for Singly Mounted Bearings when Fa by Fr is greater than 1.14

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Verified Radial Load for Back to Back Bearings when Fa by Fr greater than 1.14

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Verified Radial Load for Back to Back Bearings when Fa by Fr less than or equal to 1.14

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Verified Radial Load for Singly Mounted Bearings when Fa by Fr is greater than 1.14

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Verified Angular Frequency given Constant K and Mass

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Verified Angular Frequency given Velocity and Distance

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Verified Angular Velocity of Driven Wheel given Longitudinal Slip Velocity, Velocity of Free Rolling Wheel

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Verified Angular Velocity of Driven Wheel given Slip Ratio and Angular Velocity of Free Rolling Wheel

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Verified Angular Velocity of Free Rolling Wheel given Longitudinal Slip Velocity, Velocity of Driven Wheel

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Verified Angular Velocity of Free Rolling Wheel given Slip Ratio and Angular Velocity of Driven Wheel

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Created Angular Velocity of disc given Circumferential stress at center of solid disc

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Created Angular velocity of disc given Circumferential stress in solid disc

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Created Angular velocity of disc given Constant at boundary condition for circular disc

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Created Angular velocity of disc given maximum radial stress

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Created Angular velocity of disc given Radial stress at center of solid disc

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Created Angular Velocity of disc given Radial stress in solid disc

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Created Angular velocity of disc given Radial stress in solid disc and Outer radius

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Created Disc's Angular velocity given Circumferential stress and Outer radius

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Created Disc's angular velocity given maximum circumferential stress in solid disc

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Verified Angle between IC and Ground

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Verified Camber Change Rate

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Verified Front View Swing Arm

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Verified Height of Centre of Gravity from Road Surface from Percentage Anti Dive

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Verified Height of Centre of Gravity from Road Surface from Percentage Anti Lift

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Verified Percent Anti Squat

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Verified Percentage Anti Dive on Front

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Verified Percentage Anti Lift

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Verified Percentage Front Braking given Percentage Anti Dive

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Verified Percentage Rear Braking given Percentage Anti Lift

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Verified Roll Camber

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Verified Wheelbase of Vehicle from Percentage Anti Dive

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Verified Wheelbase of Vehicle from Percentage Anti Lift

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Verified Transformed Conical Variable with Cone Angle in Hypersonic Flow

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Verified Transformed Conical Variable with Wave Angle

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9 More Approximate Methods of Hypersonic Inviscid Flowfields Calculators

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Created Area of Double Fillet Weld given Tensile Force

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Created Area of Fillet Weld given Thickness of Plate for Single Fillet Lap Joint

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Created Area of Fillet Weld given Throat Thickness for Double Fillet Lap Joint

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Created Area of Fillet Weld given Throat Thickness for Single Fillet Lap Joint

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Created Area of Fillet Weld in given Thickness of Plate for Double Fillet Lap Joint

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Created Area of Parallel Fillet Weld given Thickness of Plate

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Created Area of Parallel Fillet Weld given Throat Thickness

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Created Area of Single Fillet Weld given Tensile Force

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Created Total Surface Area of Triangular Prism given Base Area

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7 More Area of Triangular Prism Calculators

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Created Angle between Incident Ray and Scattering Planes in X-ray Diffraction

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Verified Quantization of Angular Momentum

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Created Spacing between Atomic Lattice Planes in X-ray Diffraction

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Created Wavelength in X-ray Diffraction

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6 More Atom Calculators

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Verified Mechanical Trail

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Verified Tire Rate given Wheel Rate and Ride Rate

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Verified Total axial force

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Verified Wheel Rate given Tire Rate and Ride Rate

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5 More Automobile Calculators

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Verified Average Energy Delivered per Spark

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Verified Resistance of Charging Circuit from Average Power per Spark

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Verified Voltage of Power Supply from Average Power per Spark

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Created Average Shear Force for Circular Section

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Created Average Shear Stress for Circular Section

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Created Average Shear Stress for Circular Section given Maximum Shear Stress

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Created Axial Load of Spring for given Deflection and Stiffness of Spring

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Created Axial Load on Spring given Deflection of Spring

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Created Axial Load on Spring given Strain Energy Stored by Spring

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Created Axial Load on Spring given Work Done on Spring

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Created Axial Loading on Spring

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Created Axial Loading on Spring given Maximum Shear Stress induced in Wire

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Verified Allowable Load for given Safety Factor

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Verified Shaft Resistance using Allowable Load and Safety Factor

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Verified Toe Resistance using Allowable Load and Safety Factor

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2 More Axial Load Capacity of Single Piles Calculators

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Created Angle Made by Resultant Force with Horizontal

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Created Resultant Centrifugal Force

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Created Base Area of Cone given Lateral Surface Area and Slant Height

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6 More Base Area of Cone Calculators

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Created Base Circumference of Cone given Lateral Surface Area and Slant Height

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Created Base Circumference of Cone given Volume

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5 More Base Circumference of Cone Calculators

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Verified Reference Current of BJT Current Mirror

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Verified Short Circuit Current Gain of BJT

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12 More Base Current Calculators

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Verified Closed-Loop Gain as Function of Ideal Value

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Verified Gain with Feedback of Feedback Amplifier

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1 More Basic Characteristics Calculators

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Verified Clearance factor in compressor

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Verified Clearance Volume given Clearance Factor

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Verified Compression Ratio given Pressure

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Verified Compression Ratio given Volume

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Verified Discharge Pressure given Compression Ratio

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Verified Discharge Volume given Compression Ratio

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Verified Piston Displacement Volume given Clearance Factor

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Verified Piston Displacement Volume given Volumetric Efficiency in Compressor

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Verified Suction Pressure given Compression Ratio

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Verified Suction Volume given Compression Ratio

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Verified Suction Volume given Volumetric Efficiency in Compressor

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Verified Volumetric efficiency in compressor

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Verified Circumferential stress developed in pipe wall

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Verified Force required to accelerate water in pipe

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Verified Longitudinal Stress developed in Pipe wall

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9 More Basic Formulas Calculators

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Created Frequency of Oscillation for SHM

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Created Periodic Time for SHM

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2 More Basics Calculators

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Verified Angle of incidence of sun rays

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Verified Energy Conversion Efficiency of Solar Chimney

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Verified Hour Angle at Sunrise and Sunset

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Verified Tilt factor for diffused radiation

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Verified Tilt factor for reflected radiation

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3 More Basics Calculators

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Verified Length of Filament in 3-D printing

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5 More Basics Calculators

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Verified Static head

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14 More Basics of Centrifugal Pumps Calculators

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Verified Current Density given Electric Current and Area

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Verified Current Density given Resistivity

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Verified Electric Current given Charge and Time

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6 More Basics of Current Electricity Calculators

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Verified Equivalent Diameter of Circular Duct for Rectangular Duct when Quantity of Air is Same

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Verified Equivalent Diameter of Circular Duct for Rectangular Duct when Velocity of Air is Same

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Verified Quantity of Air given Velocity

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Verified Reynolds Number given Friction Factor for Laminar Flow

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Verified Reynolds Number in Duct

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Verified Velocity Pressure in Ducts

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Verified Decay of Current in LR circuit

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Verified Total Flux in Self Inductance

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13 More Basics of Electromagentic Induction Calculators

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Verified Diffuser Efficiency given Inlet and Exit Velocities

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16 More Basics of Gas Turbines Calculators

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Created Angle between Axis of Radius of Rotation and Line Joining Point on Curve to Origin

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Created Angle between Axis of Radius of Rotation and Line Joining Point on Curve to Origin O

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Created Corresponding Radial Force Required at Each Ball for Spring Loaded Governors

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Created Governor Power

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Created Height of Watt Governor

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Created Increased Speed

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Created Mean Equilibrium Angular Speed

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Created Mean Equilibrium Speed in RPM

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Created Ratio of Length of Arm to Length of Link

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Created Sleeve Load for Decrease in Speed Value when Taking Friction into Account

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Created Sleeve Load for Increase in Speed Value when Taking Friction into Account

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Created Speed of Rotation in RPM

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Created Total Downward Force on Sleeve in Wilson-Hartnell Governor

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Verified Number of Kanbans

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Verified Standard Error (Pooled)

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Verified Uniform Series Present Sum of Money

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10 More Basics of Industrial Engineering Calculators

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Verified Bending Stress in Shaft

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Verified Collar Friction Torque in Accordance of Uniform Pressure Theory

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Verified Design of Shaft using ASME Code

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Verified Unit Bearing Pressure

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7 More Basics of Machine Design Calculators

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Verified Maximum Convexity

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10 More Basics of Manufacturing Calculators

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Verified Number of Images in Kaleidoscope

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7 More Basics of Optics Calculators

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Verified Ride rate of car

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14 More Basics of Physics Calculators

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Verified Pressure in Bubble

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Verified Total Angle of Twist

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12 More Basics of Strength of Materials Calculators

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Verified Force on Crank Pin due to gas pressure inside cylinder

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Verified Horizontal Reaction on Bearing 3 of centre crankshaft at TDC position due to belt tension

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Verified Vertical Reaction on Bearing 1 of centre crankshaft at TDC position due to force on crank pin

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Verified Vertical Reaction on Bearing 1 of centre crankshaft at TDC position given crankweb dimension

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Verified Vertical Reaction on Bearing 2 of centre crankshaft at TDC position due to force on crank pin

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Verified Vertical Reaction on Bearing 2 of centre crankshaft at TDC position due to weight of flywheel

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Verified Vertical Reaction on Bearing 3 of centre crankshaft at TDC position due to weight of flywheel

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5 More Bearing Reactions Calculators

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Verified Horizontal Reaction on Bearing 1 of side crankshaft at TDC position by belt tension given moment

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Verified Horizontal Reaction on Bearing 1 of side crankshaft at TDC position due to belt tension

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Verified Horizontal Reaction on Bearing 2 of side crankshaft at TDC position due to belt tension

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Verified Resultant reaction at Bearing 1 of side crankshaft at TDC position

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Verified Resultant reaction at Bearing 1 of side crankshaft at TDC position given bearing pressure

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Verified Vertical Reaction on Bearing 1 of side crankshaft at TDC position due to force on crank pin

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Verified Vertical Reaction on Bearing 1 of side crankshaft at TDC position due to weight of flywheel

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Verified Vertical Reaction on Bearing 2 of side crankshaft at TDC position due to force on crank pin

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Verified Vertical Reaction on Bearing 2 of side crankshaft at TDC position due to weight of flywheel

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1 More Bearing Reactions Calculators

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Verified Vertical Reaction on Bearing 1 of side crankshaft due to radial force at max torque

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7 More Bearing Reactions Calculators

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Verified Distance between crank pin and centre crankshaft designed at max torque

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Verified Force acting on piston top due to gas pressure for maximum torque on center crankshaft

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Verified Gap of Bearing 2 from Flywheel of centre crankshaft at max torque position

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Verified Gap of Bearing 3 from Flywheel of centre crankshaft at max torque position

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Verified Horizontal Reaction on Bearing 1 of centre crankshaft due to tangential force at max torque

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Verified Horizontal Reaction on Bearing 2 of centre crankshaft due to belt tension at max torque

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Verified Horizontal Reaction on Bearing 2 of centre crankshaft due to tangential force at max torque

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Verified Horizontal Reaction on Bearing 3 of centre crankshaft due to belt tension at max torque

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Verified Resultant Reaction on Bearing 1 of centre crankshaft at angle of max torque

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Verified Resultant Reaction on Bearing 2 of centre crankshaft at angle of max torque

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Verified Resultant Reaction on Bearing 3 of centre crankshaft at angle of max torque

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Verified Tangential component of force at crank pin given horizontal reaction on bearing 1

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Verified Tangential component of force at crank pin given horizontal reaction on bearing 2

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Verified Vertical Reaction on Bearing 1 of centre crankshaft due to radial force at max torque

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Verified Vertical Reaction on Bearing 2 of centre crankshaft due to flywheel weight at max torque

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Verified Vertical Reaction on Bearing 2 of centre crankshaft due to radial force at max torque

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Verified Vertical Reaction on Bearing 3 of centre crankshaft due to flywheel weight at max torque

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1 More Bearings Reactions Calculators

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Created Angle Made by Belt with Vertical Axis for Cross Belt Drive

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Created Angle Made by Belt with Vertical Axis for Open Belt Drive

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Created Angle of Contact for Cross Belt Drive

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Created Angle of Contact for Open Belt Drive

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Created Centrifugal Tension in Belt

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Created Cross Belt Drive Length

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Created Frictional Force in V Belt Drive

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Created Initial Tension in Belt

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Verified Length of Belt that Passes over Driver

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Verified Length of Belt that Passes over Follower

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Created Length of Open Belt Drive

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Created Maximum Tension for Transmission of Maximum Power by Belt

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Created Maximum Tension of Belt

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Created Normal Reaction between Belt and Sides of Groove

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Created Power Transmitted by Belt

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Created Relation between Pitch and Pitch Circle Diameter of Chain Drive

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Created Torque Exerted on Driven Pulley

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Created Torque Exerted on Driving Pulley

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Created Total Percentage Slip in Belt

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Created Velocity for Transmission of Maximum Power by Belt

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Created Bending Moment at Center given Point Load Acting at Center of Spring Load

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Created Bending Moment at Center of Leaf Spring

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Created Bending Moment on each Plate given Total Resisting Moment by n Plates

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Created Bending Moment on Single Plate

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Created Maximum Bending Moment Developed in Plate given Bending Moment on Single Plate

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Created Maximum Bending Moment Developed in Plate given Total Resisting Moment by n Plates

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Verified Clearance between Two Shears

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5 More Bending Operation Calculators

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Verified Bending stress in lever of elliptical cross section

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Verified Bending stress in lever of elliptical cross section given bending moment

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Verified Bending stress in lever of rectangular cross section

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Verified Bending stress in lever of rectangular cross section given bending moment

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Verified Maximum bending moment in lever

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Verified Inner Diameter of Pressurized Cylinder from Bernie's Equation

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Verified Inner Diameter of Pressurized Cylinder from Clavarino's Equation

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Verified Thickness of Pressurized Cylinder from Bernie's Equation

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Verified Thickness of Pressurized Cylinder from Clavarino's Equation

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Verified Bias Current in Differential Pair

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17 More Biasing Calculators

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Created Strain in x direction in biaxial system

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Created Strain in Y direction in biaxial system

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Verified Bearing Pressure on Crank Pin Bush

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Verified Bearing Pressure on Piston Pin Bush

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Verified Crank Radius given Stroke Length of Piston

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Verified Mass of Reciprocating Parts in Engine Cylinder

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Verified Maximum Force Acting on Crank Pin Bearing given Allowable Bearing Pressure

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Verified Maximum Force Acting on Piston Pin Bearing

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Verified Maximum Force Acting on Piston Pin Bearing given Allowable Bearing Pressure

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Verified Maximum Height of Connecting Rod at Big End

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Verified Minimum Height of Connecting Rod at Big End

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3 More Big and Small End Bearings Calculators

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Verified Bending Moment on Big End Cap of Connecting Rod

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Verified Core Diameter of Bolts of Big End Cap of Connecting Rod

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Verified Inertia Force on Bolts of Connecting Rod

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Verified Mass of Connecting Rod

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Verified Maximum Bending Moment on Connecting Rod

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Verified Maximum Bending Stress in Big End Cap of Connecting Rod

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Verified Maximum Inertia Force on Bolts of Connecting Rod

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Verified Maximum Inertia Force on Bolts of Connecting Rod given Permissible Tensile Stress of Bolts

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Verified Span Length of Big End Cap of Connecting Rod

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Verified Thickness of Big End Cap of Connecting Rod given Bending Stress in Cap

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Verified Width of Big End Cap of Connecting Rod given Bending Stress in Cap

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Verified Actual Cross-sectional Area of Bolts given Root Diameter of Thread

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Verified Bolt Load in Design of Flange for Gasket Seating

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Verified Bolt load under operating condition

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Verified Bolt Load under operating condition given Hydrostatic End Force

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Verified Deflection of Spring Initial Bolt Load to Seal Gasket Joint

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Verified Gasket Width given actual Cross-sectional Area of Bolts

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Verified Hydrostatic Contact Force given Bolt Load under Operating condition

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Verified Hydrostatic end force

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Verified Hydrostatic End Force given Bolt Load under Operating condition

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Verified Initial Bolt Load to seat Gasket Joint

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Verified Load on bolts based on hydrostatic end force

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Verified Stress Required for Gasket Seating

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Verified Stress Required for Gasket Seating given Bolt Load

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Verified Test pressure given Bolt Load

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Verified Total cross-sectional area of bolt at root of thread

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Verified Width of U Collar given Initial Bolt Load to Seat Gasket Joint

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Verified Nominal Diameter of Bolt given Height of Standard Nut

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3 More Bolted Joints Calculators

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Verified Bolt Load given Flange pressure

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Verified Bolt Load given Modulus of Elasticity and Increment Length

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Verified Bolt load in gasket joint

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Verified Flange pressure developed due to tightening of bolt

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Verified Flange pressure given Twisting moment

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Verified Gasket Area given Flange pressure

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Verified Initial Bolt Torque given Bolt Load

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Verified Nominal Bolt Diameter given Bolt Load

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Verified Number of Bolts given Flange pressure

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Verified Twisting Moment given Flange Pressure

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Verified Bore of Engine Cylinder given Length

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Verified Gas Force Acting on Cylinder Cover

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Verified Indicated Mean Effective Pressure

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Verified Length of Engine Cylinder given Cylinder Bore

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Verified Length of Engine Cylinder given Stroke Length

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Verified Maximum Gas Pressure Inside Engine Cylinder

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Verified Stroke Length of Engine given Length of Cylinder

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Created Crippling Load given Moment of Section if Both Ends of Column are Fixed

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Created Crippling Load if Both Ends of Column are Fixed

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Created Deflection at Section given Moment of Section if Both Ends of Column are Fixed

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Created Length of Column given Crippling Load if Both Ends of Column are Fixed

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Created Modulus of Elasticity given Crippling Load if Both Ends of Column are Fixed

Go

Created Moment of Fixed Ends given Moment of Section if Both Ends of Column are Fixed

Go

Created Moment of Inertia given Crippling Load if Both Ends of Column are Fixed

Go

Created Moment of Section if Both Ends of Column are Fixed

Go

Created Crippling Load given Moment at Section if Both Ends of Column are Hinged

Go

Created Crippling Load when Both Ends of Column are Hinged

Go

Created Deflection at Section given Moment at Section if Both Ends of Column are Hinged

Go

Created Length of Column given Crippling Load with Both Ends of Column Hinged

Go

Created Modulus of Elasticity given Crippling Load with Both Ends of Column Hinged

Go

Created Moment due to Crippling Load at Section if Both Ends of Column are Hinged

Go

Created Moment of Inertia given Crippling Load with Both Ends of Column Hinged

Go

Created Distance of Bottom Weld from Gravity Axis given Length of Bottom Weld and Total Length of Weld

Go

Created Distance of Bottom Weld from Gravity Axis given Length of Top Weld

Go

Created Distance of Bottom Weld from Gravity Axis given Length of Top Weld and Total Length of Weld

Go

Created Distance of Bottom Weld from Gravity Axis given Moment and Length of Bottom Weld

Go

Created Distance of Bottom Weld from Gravity Axis given Moment of Bottom Weld about Gravity Axis

Go

Created Distance of Bottom Weld from Gravity Axis given Resistance of Bottom Weld

Go

Created Distance of Bottom Weld from Gravity Axis given Resistance of Bottom Weld and Total Weld Length

Go

Created Distance of Bottom Weld from Gravity Axis given Resistance of Top Weld

Go

Created Distance of Bottom Weld from Gravity Axis given Resistance of Top Weld and Total Weld Length

Go

Created Length of Bottom Weld

Go

Created Length of Bottom Weld given Area of Unsymmetrical Weld

Go

Created Length of Bottom Weld given Axial Load on Angle

Go

Created Length of Bottom Weld given Axial Load on Weld

Go

Created Length of Bottom Weld given Length of Top Weld

Go

Created Length of Bottom Weld given Moment of Bottom Weld about Gravity Axis

Go

Created Length of Bottom Weld given Resistance of Bottom Weld

Go

Created Length of Bottom Weld given Total Length of Weld

Go

Created Moment of Bottom Weld about Gravity Axis

Go

Created Moment of Bottom Weld about Gravity Axis given Resistance of Bottom Weld

Go

Created Resistance of Bottom Weld

Go

Created Resistance of Bottom Weld given Axial Load on Angle

Go

Created Resistance of Bottom Weld given Moment of Bottom Weld about Gravity Axis

Go

Created Resistance of Bottom Weld given Total Resistance

Go

Created Resistance of Bottom Weld given Total Weld Length

Go

Created Effective Radius of Drum for Simple Band Brake

Go

Created Tension in Band between First and Second Block for Band and Block Brake

Go

Created Tension in Tight Side for Band and Block Brake

Go

Created Tension in Tight Side of Band for Simple Band Brake

Go

Created Tension in Tight Side of Band for Simple Band Brake given Permissible Tensile Stress

Go

Created Brake Power of Engine for Belt Transmission Dynamometer

Go

Created Brake Power of Engine for Prony Brake Dynamometer

Go

Created Brake Power of Engine for Prony Brake Dynamometer given Speed of Shaft

Go

Created Brake Power of Engine for Prony Brake Dynamometer given Work Done per Minute

Go

Created Brake Power of Engine for Rope Brake Dynamometer

Go

Created Brake Power of Engine for Rope Brake Dynamometer if Diameter of Rope is Neglected

Go

Created Braking Torque for Band and Block Brake, Considering Thickness of Band

Go

Created Braking Torque for Band and Block Brake, Neglecting Thickness of Band

Go

Created Braking Torque for Double Block or Shoe Brake

Go

Created Braking Torque for Pivoted Block or Shoe Brake

Go

Created Braking Torque for Shoe Brake

Go

Created Braking Torque for Shoe Brake given Force Applied at End of Lever

Go

Created Braking Torque for Shoe Brake if Line of Action of Tangential Force Passes above Fulcrum Anti Clock

Go

Created Braking Torque of Shoe Brake if Line of Action of Tangential Force Passes above Fulcrum Clockwise

Go

Created Braking Torque of Shoe Brake if Line of Action of Tangential Force Passes below Fulcrum Anti Clock

Go

Created Braking Torque of Shoe Brake if Line of Action of Tangential Force Passes below Fulcrum Clockwise

Go

Created Braking Torque on Drum for Simple Band Brake Considering Band Thickness

Go

Created Braking Torque on Drum for Simple Band Brake, Neglecting Thickness of Band

Go

Verified Area Moment of Inertia for Connecting Rod Cross Section

Go

Verified Critical Buckling Load on Connecting Rod by Rankine Formula

Go

Verified Critical Buckling Load on Connecting Rod Considering Factor of Safety

Go

Verified Critical Buckling Load on Steel Connecting Rod given Thickness of Flange or Web of Connecting Rod

Go

Verified Force Acting on Connecting Rod

Go

Verified Height of Cross Section of Connecting Rod at Middle Section

Go

Verified Maximum Force Acting on Connecting Rod given Maximum Gas Pressure

Go

Verified Radius of Gyration of I Cross Section about xx Axis

Go

Verified Radius of Gyration of I Cross Section about yy Axis

Go

Verified Whipping Stress in Connecting Rod of I Cross Section

Go

Verified Width of I Cross Section of Connecting Rod

Go

Verified Transverse Shrinkage in Butt Joints

Go

13 More Butt Joints Calculators

Go

Verified Gain with Feedback at Mid and High Frequency

Go

Verified Lower 3-DB Frequency in Bandwidth Extension

Go

Verified Signal-to-Interference Ratio at Output

Go

2 More BW Extension and Signal Interference Calculators

Go

Verified By-Pass Factor of Cooling Coil

Go

Verified By-Pass Factor of Heating Coil

Go

Verified LMTD of Coil given By-Pass Factor

Go

Verified Mass of Air Passing over Coil given By-Pass Factor

Go

Verified Overall Heat Transfer Coefficient given By-Pass Factor

Go

Verified Sensible Heat given Out by Coil using By-Pass Factor

Go

Verified Surface Area of Coil given By-Pass Factor

Go

Created Condition for Maximum Acceleration of Follower Exhibiting Cycloidal Motion

Go

Created Condition for Maximum Velocity of Follower Exhibiting Cycloidal Motion

Go

Created Displacement of Follower after Time t for Cycloidal Motion

Go

Created Displacement of Follower for Circular Arc Cam, there's Contact on Circular Flank

Go

Created Mean Velocity of Follower during Outstroke at Uniform Acceleration

Go

Created Mean Velocity of Follower during Return Stroke at Uniform Acceleration

Go

Created Peripheral Speed of Projection of Point P' (Projection of Point P on Dia) for SHM of Follower

Go

Created Peripheral Speed of Projection of Point P on Diameter for SHM of Follower

Go

Created Time Required by Follower for Return Stroke at Uniform Acceleration

Go

Created Time Required for Follower during Outstroke for Uniform Acceleration

Go

Created Time Required for Out Stroke of Follower when Follower Moves with SHM

Go

Created Velocity of Follower after Time t for Cycloidal Motion

Go

Created Velocity of Follower for Circular Arc Cam if Contact is on Circular Flank

Go

Verified Capacitance of Cylindrical Capacitor

Go

Verified Capacitance of Parallel Plate Capacitor

Go

Verified Capacitance of Spherical Capacitor

Go

3 More Capacitance Calculators

Go

Verified Equivalent Resistance of Cascode Amplifier

Go

Verified Negative Voltage Gain of Cascode Amplifier

Go

Verified Open Circuit Bipolar Cascode Voltage Gain

Go

2 More Cascode Ampifier Calculators

Go

Verified Downwards Resistance of Cascode Differential Half Circuit

Go

Verified Upwards Resistance of Cascode Differential Half-Circuit

Go

Verified Voltage Gain of Cascode Differential Amplifier given Transconductance

Go

Verified Casting Yield

Go

3 More Casting Yield Calculators

Go

Created Centrifugal Force at Intermediate Position for Hartnell Governor for Maximum Force

Go

Created Centrifugal Force at Intermediate Position for Hartnell Governor for Minimum Force

Go

Created Centrifugal Force at Maximum Equilibrium Speed on Each Ball for Wilson-Hartnell Governor

Go

Created Centrifugal Force at Maximum Radius of Rotation

Go

Created Centrifugal Force at Minimum Equilibrium Speed on Each Ball for Wilson-Hartnell Governor

Go

Created Centrifugal Force at Minimum Radius of Rotation

Go

Created Centrifugal Force for Hartung Governor

Go

Created Centrifugal Force for Pickering Governor

Go

Created Centrifugal Force on Each Ball for Wilson-Hartnell Governor

Go

Created Change in diameter of thin spherical shell

Go

Created Diameter of spherical shell given change in diameter of thin spherical shells

Go

Created Diameter of thin spherical shell given strain in any one direction

Go

Created Hoop stress in thin spherical shell given strain in any one direction and Poisson's ratio

Go

Created Hoop stress induced in thin spherical shell given strain in any one direction

Go

Created Internal fluid pressure given change in diameter of thin spherical shells

Go

Created Internal fluid pressure in thin spherical shell given strain in any one direction

Go

Created Modulus of elasticity for thin spherical shell given strain and internal fluid pressure

Go

Created Modulus of elasticity given change in diameter of thin spherical shells

Go

Created Modulus of elasticity of thin spherical shell given strain in any one direction

Go

Created Poisson's ratio for thin spherical shell given strain and internal fluid pressure

Go

Created Poisson's ratio for thin spherical shell given strain in any one direction

Go

Created Poisson's ratio given change in diameter of thin spherical shells

Go

Created Strain in any one direction of thin spherical shell

Go

Created Strain in thin spherical shell given internal fluid pressure

Go

Created Thickness of spherical shell given change in diameter of thin spherical shells

Go

Created Thickness of thin spherical shell given strain in any one direction

Go

Created Change in circumference of vessel due to pressure given circumferential strain

Go

Created Change in diameter in thin cylindrical strain given volumetric strain

Go

Created Change in diameter of cylindrical shell given change in volume of cylindrical shell

Go

Created Change in diameter of thin cylindrical vessel (Circumferential strain)

Go

Created Change in diameter of vessel given internal fluid pressure

Go

Created Change in length in thin cylindrical strain given volumetric strain

Go

Created Change in length of cylindrical shell given change in volume of cylindrical shell

Go

Created Change in length of thin cylindrical shell given internal fluid pressure

Go

Created Change in length of thin cylindrical vessel given longitudinal strain

Go

Created Change in volume given circumferential strain and longitudinal strain

Go

Created Change in volume of cylindrical shell given volumetric strain

Go

Created Change in volume of thin cylindrical shell

Go

Created Change in length of Tapered Bar

Go

Verified Capacitance of Circuit from Charging Time

Go

Verified Charging Time

Go

Verified Charging Time from Minimum Resistance

Go

Verified Inductance of Circuit from Charging Time

Go

Verified Minimum Resistance from Charging Time

Go

Verified Charging Voltage for Maximum Power of Spark

Go

Verified Power Supply for Maximum Power of Spark

Go

6 More Charging voltage Calculators

Go

Verified Chip break distance when material constant is unity

Go

Verified Chip breaker distance given radius of chip curvature

Go

2 More Chip Break distance Calculators

Go

Verified Chip thickness given length of chip tool contact

Go

Verified Radius of chip curvature given constant of material

Go

2 More Chip control Calculators

Go

Verified Central angle for Portion of Curve Approximate for Chord definition

Go

Verified Central Angle for Portion of Curve Exact for Arc definition

Go

Verified Central Angle of Curve for given Length of Curve

Go

Verified Central Angle of Curve for given Length of Long Chord

Go

Verified Central Angle of Curve for given Tangent Distance

Go

Verified Degree of Curve for given Length of Curve

Go

Verified Degree of Curve for given Radius of Curve

Go

Verified Degree of Curve when Central Angle for Portion of Curve

Go

Verified Exact Length of Curve

Go

Verified Exact Tangent Distance

Go

Verified External Distance

Go

Verified Length of Curve given Central Angle for portion of Curve

Go

Verified Length of Curve or Chord by Central Angle given Central Angle for Portion of Curve

Go

Verified Length of Long Chord

Go

Verified Radius of Curve

Go

Verified Radius of Curve Exact for Chord

Go

Verified Radius of Curve given Length of Long Chord

Go

Verified Radius of Curve using Degree of Curve

Go

Verified Radius of Curve using External Distance

Go

Verified Radius of Curve using Midordinate

Go

Verified Radius of Curve using Tangent Distance

Go

6 More Circular Curves on Highways and Roads Calculators

Go

Verified Circular Orbital Radius

Go

Verified Circular Orbital Radius Given Time Period of Circular Orbit

Go

Verified Circular Orbital Radius Given Velocity of Circular Orbit

Go

Verified Escape Velocity given Speed of Satellite in Circular Orbit

Go

Verified Orbital Radius Given Specific Energy of Circular Orbit

Go

Verified Specific Energy of Circular Orbit

Go

Verified Specific Energy of Circular Orbit Given Orbital Radius

Go

Verified Speed of Satellite in Circular LEO as Function of Altitude

Go

Verified Time Period of Circular Orbit

Go

Verified Velocity of Circular Orbit

Go

Created Diameter of Circular Section given Distance of Outermost Layer from Neutral Layer

Go

Created Diameter of Circular Section given Moment of Inertia about Neutral Axis

Go

Created Diameter of Circular Section given Section Modulus

Go

Created Distance of Outermost Layer from Neutral Layer in Circular Sections

Go

Created Moment of Inertia about Neutral Axis for Circular Section

Go

Created Section Modulus for Circular Section

Go

Verified Circulation for rotating cylinders

Go

3 More Circulation Calculators

Go

Created Circumferential strain for rotating thin disc

Go

Created Circumferential strain for rotating thin disc given radius of disc

Go

Created Circumferential strain on disc given stresses

Go

Created Circumferential stress given circumferential strain on disc

Go

Created Circumferential stress given initial radial width of disc

Go

Created Circumferential stress given radial strain on disc

Go

Created Circumferential stress given radius of disc

Go

Verified Bias Current of Emitter Follower

Go

Verified Drain Current of Class B Amplifier

Go

Verified Instantaneous Power Dissipation of Emitter-Follower

Go

Verified Load Power of Output Stage

Go

Verified Load Voltage

Go

Verified Peak Output Voltage Value at Average Load Power

Go

Verified Power Conversion Efficiency of Class A Output Stage

Go

Verified Power Output Capability Factor

Go

Verified Saturation Voltage between Collector-Emitter at Transistor 1

Go

Verified Saturation Voltage between Collector-Emitter at Transistor 2

Go

Verified Supply Power of Output Stage

Go

Verified Efficiency of Class A

Go

Verified Efficiency of Class B Output Stage

Go

Verified Load Resistance of Class B Stage

Go

Verified Maximum Average Power from Class B Output Stage

Go

Verified Maximum Power Dissipation in Class B Stage

Go

Verified Negative Half of Maximum Power Dissipation in Class B Stage

Go

Verified XOR Voltage NAND Gate

Go

16 More CMOS Time Characteristics Calculators

Go

Created Coefficient of Fluctuation of Energy given Work Done per Cycle

Go

Created Coefficient of Fluctuation of Speed for Flywheel

Go

Created Coefficient of Fluctuation of Speed for Flywheel given Angular Speed and Mean Speed

Go

Created Coefficient of Fluctuation of Speed for Flywheel given Angular Velocity

Go

Created Coefficient of Fluctuation of Speed for Flywheel given Linear Velocity

Go

Created Coefficient of Fluctuation of Speed for Flywheel given Mean Angular Velocity

Go

Created Coefficient of Fluctuation of Speed for Flywheel given Mean Linear Velocity

Go

Verified Allowable Design Strength

Go

Verified Nominal Strength using Allowable Design Strength

Go

13 More Cold Formed or Light Weighted Steel Structures Calculators

Go

Created Cross Sectional Area of Column given Maximum Stress for Column with Eccentric Load

Go

Created Eccentric Load given Deflection at Section of Column with Eccentric Load

Go

Created Eccentricity given Deflection at Free End of Column with Eccentric load

Go

Created Eccentricity given Deflection at Section of Column with Eccentric load

Go

Created Eccentricity given Maximum Stress for Column with Eccentric Load

Go

Created Eccentricity given Moment at Section of Column with Eccentric Load

Go

Created Effective Length of Column given Maximum Stress for Column with Eccentric Load

Go

Created Maximum Stress for Column with Eccentric Load

Go

Created Modulus of Elasticity given Deflection at Free End of Column with Eccentric Load

Go

Created Modulus of Elasticity given Deflection at Section of Column with Eccentric Load

Go

Created Modulus of Elasticity given Maximum Stress for Column with Eccentric Load

Go

Created Moment at Section of Column with Eccentric Load

Go

Created Moment of Inertia given Deflection at Free End of Column with Eccentric Load

Go

Created Moment of Inertia given Deflection at Section of Column with Eccentric Load

Go

Created Moment of Inertia given Maximum Stress for Column with Eccentric Load

Go

Created Section Modulus given Maximum Stress for Column with Eccentric Load

Go

Created Crippling Load given Factor of Safety

Go

Created Crippling Load given Final Deflection at Distance X from end A of Column

Go

Created Crippling Load given Maximum Deflection for Columns with Initial Curvature

Go

Created Distance from Neutral Axis of Extreme Layer given Maximum Stress for Columns

Go

Created Euler Load

Go

Created Euler Load given Factor of Safety

Go

Created Euler Load given Final Deflection at Distance X from end A of Column

Go

Created Euler Load given Maximum Deflection for Columns with Initial Curvature

Go

Created Euler Stress given Maximum Stress for Columns with Initial Curvature

Go

Created Factor of Safety given Euler Load

Go

Created Length of Column given Euler Load

Go

Created Length of Column given Final Deflection at Distance X from End A of Column

Go

Created Length of Column given Initial Deflection at Distance X from end A

Go

Created Maximum Stress for Columns with Initial Curvature

Go

Created Modulus of Elasticity given Euler Load

Go

Created Moment of Inertia given Euler Load

Go

Created Radius of Gyration given Maximum Stress for Columns with Initial Curvature

Go

Created Value of Distance 'X' given Final Deflection at Distance X from end A of Column

Go

Created Value of Distance 'X' given Initial Deflection at Distance X from end A

Go

Verified Common-Mode Signal of MOSFET given Resistance

Go

9 More Common Mode Rejection Ratio (CMRR) Calculators

Go

Verified Common Mode Input Resistance of BJT Half-Circuit

Go

Verified Common Mode Rejection Ratio of BJT

Go

1 More Common Mode Rejection Ratio (CMRR) Calculators

Go

Verified Total Current Gain with respect to Voltage Gain

Go

7 More Common-Base Amplifier Calculators

Go

Verified Output Resistance of Emitter-Degenerated CE Amplifier

Go

7 More Common-Emitter Amplifier Calculators

Go

Verified Current Gain of Controlled Source Transistor

Go

Verified Output Resistance at Another Drain of Controlled Source Transistor

Go

Verified Output Resistance of CS Amplifier with Source Resistance

Go

Verified Output Voltage of Controlled Source Transistor

Go

Verified Total Voltage Gain of CS Amplifier

Go

Verified Transconductance in Common Source Amplifier

Go

5 More Common-Source Amplifier Calculators

Go

Created Constant 'a' for inner cylinder given original difference of radii at junction

Go

Created Constant for outer cylinder given original difference of radii at junction

Go

Created Decrease in outer radius of inner cylinder at junction given constants of lame equation

Go

Created Decrease in outer radius of inner cylinder at junction of compound cylinder

Go

Created Hoop stress given decrease in outer radius of inner cylinder

Go

Created Hoop stress given increase in inner radius of outer cylinder

Go

Created Increase in inner radius of outer cylinder at junction given constants of lame equation

Go

Created Increase in inner radius of outer cylinder at junction of compound cylinder

Go

Created Mass of compound cylinder given decrease in outer radius of inner cylinder

Go

Created Mass of compound cylinder given increase in inner radius of outer cylinder

Go

Created Modulus of elasticity decrease in outer radius of inner cylinder

Go

Created Modulus of elasticity given decrease in outer radius of inner cylinder and constants

Go

Created Modulus of elasticity given increase in inner radius of outer cylinder

Go

Created Modulus of elasticity given increase in inner radius of outer cylinder and constants

Go

Created Modulus of elasticity given original difference of radii at junction

Go

Created Original difference of radii at junction

Go

Created Radial pressure given decrease in outer radius of inner cylinder

Go

Created Radial pressure given increase in inner radius of outer cylinder

Go

Created Radius at junction of compound cylinder given decrease in outer radius of inner cylinder

Go

Created Radius at junction of compound cylinder given increase in inner radius of outer cylinder

Go

Created Radius at junction of compound cylinder given original difference of radii at junction

Go

Created Frequency of Compound Pendulum in SHM

Go

Created Minimum Periodic Time of SHM for Compound Pendulum

Go

Created Periodic Time of SHM for Compound Pendulum given Radius of Gyration

Go

Verified Emissivity given Reference Temperature

Go

Verified Freestream Density given Reference Temperature

Go

Verified Nose Radius of Coordinate System

Go

Verified Nose Radius of Coordinate System given Reference Temperature

Go

Verified Reference Temperature given Emissivity

Go

Verified Reference Temperature given Freestream Velocity

Go

Verified Reference Viscosity Given Reference Temperature

Go

4 More Computational Fluid Dynamic Solutions Calculators

Go

Verified Collector efficiency factor concentrating collector

Go

Verified Heat removal factor concentrating collector

Go

Verified Outer Diameter of Absorber Tube given Concentration Ratio

Go

Verified Useful heat gain when collection efficiency is present

Go

Verified Useful heat gain when collector efficiency factor is present

Go

18 More Concentrating Collectors Calculators

Go

Verified Axial Force transmitted by Inner Spring

Go

10 More Concentric Springs Calculators

Go

Verified Cost Index given Minimum Design Index

Go

Verified Landing weight given take off weight and mission fuel weight

Go

Verified Landing weight given zero fuel weight and reserve fuel weight

Go

Verified Maximum payload capability

Go

Verified Maximum take off weight

Go

Verified Minimum design index

Go

Verified Mission fuel given take off, reserve and zero fuel weight

Go

Verified Payload weight from Unity equation

Go

Verified Period of Design Index given Minimum Design Index

Go

Verified Take off weight from Unity equation

Go

Verified Take off weight given reserve, mission and zero fuel weight

Go

Verified Zero fuel weight given mission fuel, reserve and take off weight

Go

Verified Zero fuel weight given reserve and landing weight

Go

11 More Conceptual Design Calculators

Go

Verified Heat Rejection Factor

Go

4 More Condensers Calculators

Go

Verified Conduction through Edge of Two Adjoining Walls of Equal Thickness

Go

Verified Eccentric Isothermal Cylinder in Cylinder of Same Length

Go

Verified Isothermal Cylinder at Center of Square Solid Bar of Same Length

Go

Verified Long Hollow Cylindrical Layer

Go

Verified Square Flow Passage with Width to b Ratio Greater than 1.4

Go

Verified Square Flow Passage with Width to b Ratio Less than 1.4

Go

3 More Conduction Shape Factors for Different Configurations Calculators

Go

Created Constant 'a' for inner cylinder given hoop stress at radius x

Go

Created Constant 'a' for inner cylinder given radial pressure at junction of two cylinders

Go

Created Constant 'a' for inner cylinder given radial pressure at radius x

Go

Created Constant 'a' for outer cylinder given hoop stress at radius x

Go

Created Constant 'a' for outer cylinder given hoop stress at radius x and constant b

Go

Created Constant 'a' for outer cylinder given outer radius of cylinder

Go

Created Constant 'a' for outer cylinder given radial pressure at junction of two cylinders

Go

Created Constant 'a' for outer cylinder given radial pressure at radius x

Go

Created Constant A for single thick shell given hoop stress due to internal fluid pressure alone

Go

Created Constant A for single thick shell given outer radius of compound cylinder

Go

Created Constant A for single thick shell given Radial pressure due to internal fluid pressure alone

Go

Created Constant A for single thick shell of compound cylinder given internal fluid pressure

Go

Created Constant 'b' for inner cylinder given hoop stress at radius x

Go

Created Constant 'b' for inner cylinder given outer radius of cylinder

Go

Created Constant 'b' for inner cylinder given radial pressure at junction of two cylinders

Go

Created Constant 'b' for inner cylinder given radial pressure at radius x

Go

Created Constant 'b' for outer cylinder given hoop stress at radius x

Go

Created Constant 'b' for outer cylinder given outer radius of cylinder

Go

Created Constant 'b' for outer cylinder given radial pressure at junction of two cylinders

Go

Created Constant 'b' for outer cylinder given radial pressure at radius x

Go

Created Constant B for single thick shell given hoop stress due to internal fluid pressure alone

Go

Created Constant B for single thick shell given outer radius of compound cylinder

Go

Created Constant B for single thick shell given Radial pressure due to internal fluid pressure alone

Go

Created Constant B for single thick shell of compound cylinder given internal fluid pressure

Go

Created Constant for inner cylinder given outer radius of cylinder

Go

Verified Cross-Sectional Area of Duct at Section 1 using Continuity Equation

Go

Verified Cross-Sectional Area of Duct at Section 2 using Continuity Equation

Go

Verified Velocity of Air at Duct Section 1 using Continuity Equation

Go

Verified Velocity of Air at Duct Section 2 using Continuity Equation

Go

Verified Moment produced by vertical tail for given lift curve slope

Go

Verified Sideslip angle for given moment produced by vertical tail

Go

Verified Vertical tail angle of attack for given vertical tail side force

Go

Verified Vertical tail area for given vertical tail side force

Go

Verified Vertical tail dynamic pressure for given vertical tail side force

Go

Verified Vertical tail lift curve slope

Go

Verified Vertical tail lift curve slope for given moment

Go

Verified Vertical tail moment arm for given lift curve slope

Go

Verified Vertical tail Side force

Go

6 More Contribution of Aircraft Components- Part 1 Calculators

Go

Verified Dynamic pressure at vertical tail for given yawing moment coefficient

Go

Verified Sideslip angle for given yawing moment coefficient

Go

Verified Sidewash angle for given moment produced by vertical tail

Go

Verified Sidewash Angle given Yawing Moment Coefficient using Wingspan

Go

Verified Vertical tail area for given moment

Go

Verified Vertical tail area for given yawing moment coefficient

Go

Verified Vertical tail dynamic pressure for given moment

Go

Verified Vertical tail lift curve slope for given yawing moment coefficient

Go

Verified Yawing moment coefficient for given vertical tail lift curve slope

Go

5 More Contribution of Aircraft Components- Part 2 Calculators

Go

Verified Dynamic pressure at wing for given yawing moment coefficient

Go

Verified Vertical tail efficiency for given yawing moment coefficient

Go

Verified Vertical tail lift curve slope for given yawing moment coefficient and Vertical Tail Efficiency

Go

Verified Vertical tail volume ratio for given yawing moment coefficient

Go

Verified Wing area for given yawing moment coefficient

Go

Verified Wingspan for yawing moment coefficient given sideslip angle and sidewash angle

Go

Verified Yawing moment coefficient for given vertical tail volume ratio

Go

8 More Contribution of Aircraft Components- Part 3 Calculators

Go

Verified Sideslip angle for yawing moment coefficient given vertical tail volume ratio

Go

Verified Sidewash angle for given yawing moment coefficient

Go

Created Relation between Controlling Force and Radius of Rotation for Isochronous Governor

Go

Created Relation between Controlling Force and Radius of Rotation for Stable Governor

Go

Created Relation between Controlling Force and Radius of Rotation for Unstable Governor

Go

Created Value of Controlling Force for Decrease in Speed

Go

Created Value of Controlling Force for Increase in Speed

Go

Verified Bare area over fin leaving fin base given convection coefficient

Go

Verified Convection Coefficient based on Inside Area

Go

Verified Effective convection coefficient on outside given convection coefficient

Go

Verified Fin efficiency given convection coefficient

Go

Verified Height of tube tank given convection coefficient

Go

Verified Inner diameter of tube given convection coefficient

Go

Verified Surface area of fin given convection coefficient

Go

3 More Convection Coefficient Calculators

Go

Verified Average Sherwood Number of Combined Laminar and Turbulent Flow

Go

Verified Average Sherwood Number of Flat Plate Turbulent Flow

Go

Verified Average Sherwood Number of Internal Turbulent Flow

Go

Verified Density of material given convective heat and mass transfer coefficient

Go

Verified Drag coefficient of flat plate in combined laminar turbulent flow

Go

Verified Heat Transfer Coefficient for Simultaneous Heat and Mass Transfer

Go

Verified Mass Transfer Boundary Layer Thickness of Flat Plate in Laminar Flow

Go

Verified Mass Transfer Stanton Number

Go

Verified Partial pressure of component A in mixture 1

Go

Verified Specific heat given convective heat and mass transfer

Go

9 More Convective Mass Transfer Calculators

Go

Verified Cooling load from lighting

Go

10 More Cooling Loads Calculators

Go

Verified Core Diameter of Bolt given Shear Area of Nut

Go

Verified Core Diameter of Bolt given Tensile Force on Bolt in Shear

Go

2 More Core Diameter Calculators

Go

Verified Core diameter of Bolt given Tensile Stress

Go

3 More Core Diameter Calculators

Go

Verified Buoyant Force on Cores

Go

Verified Volume of Core

Go

11 More Cores - Core Prints and Chaplets Calculators

Go

Verified Maximum Spark Current to be Maintained Indefinitely

Go

Verified Power Supply for Maintaining Maximum Sparking Current

Go

Verified Resistance of Circuit using Arcing Criteria

Go

Verified Spark Discharge Voltage at Maximum Spark Current

Go

Created Additional Deflection of Centre of Gravity of Rotor using Natural Circular Frequency

Go

Created Additional Deflection of Centre of Gravity of Rotor using Whirling Speed

Go

Created Additional Deflection of Centre of Gravity of Rotor when Shaft Starts Rotating

Go

Created Centrifugal Force Causing Shaft Deflection

Go

Created Critical or Whirling Speed given Static Deflection

Go

Created Critical or Whirling Speed given Stiffness of Shaft

Go

Created Critical or Whirling Speed in R.P.S

Go

Created Force Resisting Additional Deflection of Centre of Gravity of Rotor

Go

Created Mass of Rotor given Centrifugal Force

Go

Created Natural Circular Frequency of Shaft

Go

Created Static Deflection of Shaft

Go

Created Stiffness of Shaft for Equilibrium Position

Go

Verified Cross Sectional Area for given Dynamic Thrust Exerted by Jet on Plate

Go

Verified Cross Sectional Area for given Normal Thrust Normal to Direction of Jet

Go

Verified Cross Sectional Area for given Work Done by Jet per Second

Go

1 More Cross sectional area Calculators

Go

Verified Cross Section Area of Socket End Resisting Shear Failure

Go

Verified Cross Section Area of Socket of Cotter Joint Prone to Failure

Go

Verified Cross Section Area of Spigot of Cotter Joint Prone to Failure

Go

Created Debye Temperature

Go

Verified Current in Common-Mode Rejection of MOSFET

Go

Verified Drain Current of MOSFET on Large-Signal Operation given Overdrive Voltage

Go

Verified Second Drain Current of MOSFET on Large-Signal Operation given Overdrive Voltage

Go

Verified Short Circuit Current of MOSFET

Go

8 More Current Calculators

Go

Verified Base Current of Input Differential BJT Amplifier

Go

Verified Base Current of Input Differential BJT Amplifier given Emitter Resistance

Go

Verified Collector Current of BJT Differential Amplifier given Emitter Current

Go

Verified Collector Current of BJT Differential Amplifier given Emitter Resistance

Go

Verified First Collector Current of BJT Differential Amplifier

Go

Verified First Emitter Current of BJT Differential Amplifier

Go

Verified Input Bias Current of Differential Amplifier

Go

Verified Maximum Input Common-Mode Range Voltage of BJT Differential Amplifier

Go

Verified Second Collector Current of BJT Differential Amplifier

Go

Verified Second Emitter Current of BJT Differential Amplifier

Go

1 More Current and Voltage Calculators

Go

Verified Current Density given Conductivity

Go

2 More Current Density Calculators

Go

Verified Feed given Roughness value

Go

Verified Roughness value of tool

Go

Verified Working major cutting edge Angle given Roughness value

Go

Verified Working minor cutting edge Angle given Roughness value

Go

10 More Cutting fluid and Surface Roughness Calculators

Go

Verified Cutting Force for Frictional Force along Tool Rake Face and Thrust Force

Go

Verified Cutting Force given Shear Force and Thrust Force

Go

4 More Cutting Force Calculators

Go

Verified Core Diameter of Studs

Go

Verified Core Diameter of Studs given Nominal Diameter

Go

Verified Maximum Number of Studs for Cylinder Head

Go

Verified Maximum Pitch of Studs for Cylinder Head

Go

Verified Minimum Number of Studs for Cylinder Head

Go

Verified Minimum Pitch of Studs for Cylinder Head

Go

Verified Net Resisting Force Offered by Cylinder Head Studs

Go

Verified Nominal Diameter of Studs

Go

Verified Pitch Circle Diameter of Studs

Go

Verified Pitch Circle Diameter of Studs given Pitch and Number of Studs

Go

Verified Pitch of Englne Cylinder Head Studs

Go

Verified Thickness of Cylinder Head

Go

Verified Width of Grinding path given number of workpiece revolutions

Go

16 More Cylindrical Grinding cycle Calculators

Go

Verified Current on Operation with Differential Input Voltage

Go

Verified Maximum Differential Input Voltage of MOSFET given Overdrive Voltage

Go

Verified Offset Voltage of MOSFET with Current-Mirror Load

Go

1 More DC Offset Calculators

Go

Verified Input Offset Current of Differential Amplifier

Go

3 More DC Offset Calculators

Go

Verified Dedendum Circle Diameter of Large Size Gear

Go

4 More Dedendum Circle Diameter Calculators

Go

Created Deflection at Free End given Deflection at Section of Column with Eccentric load

Go

Created Deflection at Free End given Moment at Section of Column with Eccentric load

Go

Created Deflection at Free End of Column with Eccentric load

Go

Created Deflection at Section of Column with Eccentric Load

Go

Created Deflection at Section of Column with Eccentric Load given Moment at Section

Go

Created Distance of Section from Fixed End given Deflection at Section of Column with Eccentric Load

Go

Created Final Deflection at Distance X from end A of Column

Go

Created Initial Deflection at Distance X from end A

Go

Created Maximum Deflection for Columns with Initial Curvature

Go

Created Maximum Initial Deflection given Final Deflection at Distance X from End A of Column

Go

Created Maximum Initial Deflection given Initial Deflection at Distance X from A

Go

Created Maximum Initial Deflection given Maximum Deflection for Columns with Initial Curvature

Go

Created Maximum Initial Deflection given Maximum Stress for Columns with Initial Curvature

Go

Verified Degree of Saturation given Partial Pressure of Water Vapour

Go

Verified Degree of Saturation given Relative Humidity

Go

Verified Degree of Saturation given Specific Humidity

Go

Verified Partial Pressure of Water Vapor in Saturated Air given Degree of Saturation

Go

Verified Total Pressure of Moist Air given Degree of Saturation

Go

Created Density of disc material given Radial stress in solid disc and outer radius

Go

Created Density of material given Circumferential stress and Outer radius

Go

Created Density of material given Circumferential stress at center of solid disc

Go

Created Density of material given Circumferential stress in solid disc

Go

Created Density of material given constant at boundary condition for circular disc

Go

Created Density of material given maximum circumferential stress in solid disc

Go

Created Density of material given maximum radial stress in solid disc

Go

Created Density of material given Radial stress at center of solid disc

Go

Created Density of material given Radial stress in solid disc

Go

Verified Depth of Groove given Allowable Impact Loading on Groove

Go

Verified Depth of Groove given Allowable Static Thrust Load and Allowable Impact Loading on Groove

Go

Verified Depth of Groove given allowable Static Thrust Load on Groove

Go

Verified Depth of Groove given Allowable Static Thrust Load on Ring which is Subject to Shear

Go

Verified Bearing pressure at bearing1 of side crankshaft at TDC position

Go

Verified Bending moment in shaft at bearing1 of side crankshaft at TDC position

Go

Verified Bending stress in shaft at bearing1 of side crankshaft at TDC position

Go

Verified Diameter of journal at bearing1 of side crankshaft at TDC position

Go

Verified Diameter of shaft at bearing1 of side crankshaft at TDC position

Go

Verified Length of Bearing 1 of Side Crankshaft at TDC Position given Bending Moment at Bearing

Go

Verified Length of bearing1 of side crankshaft at TDC position

Go

Verified Length of crankpin given bending moment at bearing 1 of side crankshaft at TDC position

Go

Verified Maximum length of Bearing 1 of side crankshaft at TDC position given crankpin diameter

Go

Verified Minimum length of Bearing 1 of side crankshaft at TDC position given crankpin diameter

Go

Verified Overhang Distance of piston force from Bearing 1 of side crankshaft at TDC position

Go

3 More Design of Bearings Calculators

Go

Verified Actual Number of Teeth on Bevel Gear

Go

Verified Axial or Thrust Component of Force on Bevel Gear

Go

Verified Back Cone Radius of Bevel Gear

Go

Verified Beam Strength of Tooth of Bevel Gear

Go

Verified Cone Distance of Bevel Gear

Go

Verified Material Constant for Bevel Gear Wear Strength

Go

Verified Radial Force Component acting on Bevel Gear

Go

Verified Radius of Pinion at Midpoint along Face Width for Bevel Gear

Go

Verified Radius of Pinion at Midpoint given Torque and Tangential Force for Bevel Gear

Go

Verified Tangential Force on Bevel Gear Teeth

Go

Verified Velocity Factor for Cut Teeth of Bevel Gear

Go

Verified Velocity Factor for Generated Teeth of Bevel Gear

Go

Verified Virtual or Formative Number of Teeth of Bevel Gear

Go

Verified Wear Strength of Bevel Gear by Buckingham's Equation

Go

3 More Design of Bevel Gear Calculators

Go

Verified Allowable Shear Stress in Pins of Coupling

Go

Verified Torque Transmitted by Coupling given Outer Bush Diameter

Go

13 More Design of Bushed-Pin Flexible Coupling Calculators

Go

Verified Diameter of Driving Shaft of Muff Coupling given Outer Diameter of Sleeve

Go

Verified Outer Diameter of Sleeve of Muff Coupling

Go

Verified Tensile Force on Each Bolt of Clamp Coupling

Go

Verified Tensile Force on Each Bolt of Clamp Coupling given Torque

Go

6 More Design of Clamp and Muff Coupling Calculators

Go

Verified Bending Moment at centre plane of crank pin of centre crankshaft at TDC position

Go

Verified Bending Moment at centre plane of crankpin of centre crankshaft at TDC position given bending stress

Go

Verified Bending stress in crank pin of centre crankshaft at TDC position given diameter of crank pin

Go

Verified Diameter of crank pin of centre crankshaft at TDC position given allowable bearing pressure

Go

Verified Diameter of crank pin of centre crankshaft at TDC position given bending stress and bending moment

Go

Verified Diameter of crank pin of centre crankshaft at TDC position given thickness of crank web

Go

Verified Diameter of crank pin of centre crankshaft at TDC position given width of crank web

Go

Verified Force on crank pin given crank pin length, diameter and bearing pressure

Go

Verified Length of crank pin of centre crankshaft at TDC position given allowable bearing pressure

Go

Verified Bearing pressure at crank pin bush of centre crankshaft for max torque

Go

Verified Bending moment at central plane of crank pin of centre crankshaft at max torque

Go

Verified Diameter of crank pin of centre crankshaft for max torque

Go

Verified Diameter of crank pin of centre crankshaft for max torque given bending and torsional moment

Go

Verified Length of crank pin of centre crankshaft for max torque given allowable bearing pressure

Go

Verified Torsional moment at central plane of crank pin of centre crankshaft at max torque

Go

2 More Design of Crank Pin Calculators

Go

Verified Bending stress in crank pin of side crankshaft at max torque given crankpin diameter

Go

Verified Diameter of crankpin given mean bending stress in crankpin

Go

Verified Length of crankpin given mean bending moment in crankpin

Go

Verified Maximum bending moment in crankpin when load acts at end point on crankpin as cantilever beam

Go

Verified Maximum bending moment in crankpin when load is uniformly distributed along length as cantilever

Go

Verified Maximum length of crankpin given crankpin diameter

Go

Verified Mean bending moment in crankpin

Go

Verified Minimum length of crankpin given crankpin diameter

Go

Verified Section modulus of crankpin

Go

2 More Design of Crank Pin Calculators

Go

Verified Bending Moment in horizontal plane of crank pin of side crankshaft at max torque

Go

Verified Bending Moment in vertical plane of crank pin of side crankshaft at max torque

Go

Verified Resultant Bending Moment in crank pin of side crankshaft at max torque

Go

Verified Resultant Bending Moment in crank pin of side crankshaft at max torque given crankpin diameter

Go

Verified Bending moment at central plane of crank web of centre crankshaft at TDC position

Go

Verified Bending stress at central plane of crank web of centre crankshaft at TDC position

Go

Verified Direct compressive stress in central plane of crank web of centre crankshaft at TDC position

Go

Verified Maximum Bending stress in crank web of centre crankshaft at TDC position given bending moment

Go

Verified Thickness of crank web of centre crankshaft at TDC position given bearing pressure for crank pin

Go

Verified Thickness of crank web of centre crankshaft at TDC position given bending moment in crank pin

Go

Verified Thickness of crank web of centre crankshaft at TDC position given diameter of crank pin

Go

Verified Thickness of crank web of centre crankshaft at TDC position given width of crank web

Go

Verified Total compressive stress at central plane of crank web of centre crankshaft at TDC position

Go

Verified Width of crank web of centre crankshaft at TDC position given bearing pressure for crank pin

Go

Verified Width of crank web of centre crankshaft at TDC position given bending moment in crank pin

Go

Verified Width of crank web of centre crankshaft at TDC position given compressive stress

Go

Verified Width of crank web of centre crankshaft at TDC position given diameter of crank pin

Go

Verified Width of crank web of centre crankshaft at TDC position given thickness of crank web

Go

1 More Design of Crank Web Calculators

Go

Verified Maximum compressive stress in crankweb of centre crankshaft for max torque given direct stress

Go

Verified Polar section modulus of crankweb of centre crankshaft for max torque

Go

Verified Section modulus of crankweb of centre crankshaft for max torque

Go

Verified Shear stress in crankweb of centre crankshaft for max torque given polar section modulus

Go

Verified Shear stress in crankweb of centre crankshaft for max torque given torsional moment

Go

Verified Torsional moment in crankweb of centre crankshaft for max torque given reaction on bearing1

Go

Verified Torsional moment in crankweb of centre crankshaft for max torque given reaction on bearing2

Go

Verified Torsional moment in crankweb of centre crankshaft for max torque given shear stress

Go

12 More Design of Crank Web Calculators

Go

Verified Bending moment in central plane of crankweb

Go

Verified Bending stress in central plane of crankweb

Go

Verified Bending stress in central plane of crankweb given bending moment

Go

Verified Direct compressive stress in central plane of crankweb of side crankshaft at TDC Position

Go

Verified Length of crankpin given bending moment in central plane of crankweb

Go

Verified Length of crankpin given bending stress in central plane of crankweb

Go

Verified Thickness of crankweb given bending moment at bearing 1 of side crankshaft at TDC position

Go

Verified Thickness of crankweb given bending moment in central plane of crankweb

Go

Verified Total compressive stress in central plane of crankweb of side crankshaft at TDC position

Go

Verified Bending moment in crankweb of side crankshaft due to radial thrust for max torque given stress

Go

Verified Bending moment in crankweb of side crankshaft due to radial thrust for maximum torque

Go

Verified Bending moment in crankweb of side crankshaft due to tangential thrust for max torque

Go

Verified Bending moment in crankweb of side crankshaft due to tangential thrust for max torque given stress

Go

Verified Bending stress in crankweb of side crankshaft due to radial thrust for max torque

Go

Verified Bending stress in crankweb of side crankshaft due to radial thrust for max torque given moment

Go

Verified Bending stress in crankweb of side crankshaft due to tangential thrust for max torque

Go

Verified Bending stress in crankweb of side crankshaft due to tangential thrust for max torque given moment

Go

Verified Maximum compressive stress in crankweb of side crankshaft for max torque

Go

5 More Design of Crank Web Calculators

Go

Verified Bearing pressure of journal at bearing 2 of centre crankshaft for max torque

Go

Verified Diameter of journal at bearing 2 of centre crankshaft for max torque

Go

Verified Length of journal at bearing 2 of centre crankshaft for max torque

Go

Verified Area Moment of Inertia of Cross Section of Rocker Arm

Go

Verified Area Moment of Inertia of Cross Section of Rocker Arm given Bending Stress and Moment

Go

Verified Diameter of Fulcrum Pin of Rocker Arm given Bending Moment near Boss of Rocker Arm

Go

Verified Length of Rocker Arm of Exhaust Valve Side

Go

3 More Design of Cross Section of Rocker Arm Calculators

Go

Verified Area of cross section of curved beam given bending stress at inner fiber

Go

Verified Area of cross section of curved beam given bending stress at outer fiber

Go

Verified Bending moment at fibre of curved beam given bending stress and eccentricity

Go

Verified Bending moment at fibre of curved beam given bending stress and radius of centroidal axis

Go

Verified Bending moment in curved beam given bending stress at inner fibre

Go

Verified Bending moment in curved beam given bending stress at outer fibre

Go

Verified Bending stress at inner fibre of curved beam given bending moment

Go

Verified Bending stress at outer fibre of curved beam given bending moment

Go

Verified Bending stress in fibre of curved beam given eccentricity

Go

Verified Bending stress in fibre of curved beam given radius of centroidal axis

Go

Verified Diameter of circular curved beam given radius of centroidal axis

Go

Verified Distance of fibre from neutral axis of rectangular curved beam given inner and outer fiber radius

Go

Verified Distance of fibre from neutral axis of rectangular curved beam given radius of centroidal axis

Go

Verified Distance of inner fiber from neutral axis of curved beam given bending stress at fibre

Go

Verified Distance of outer fibre from neutral axis of curved beam given bending stress at fibre

Go

Verified Eccentricity between centroidal and neutral axis of curved beam given bending stress at inner fibre

Go

Verified Eccentricity between centroidal and neutral axis of curved beam given bending stress at outer fibre

Go

Verified Eccentricity between centroidal and neutral axis of curved beam given radius of both axis

Go

2 More Design of Curved Beams Calculators

Go

Verified Maximum Radial or Tensile Stress in Flywheel

Go

Verified Moment of Inertia of Flywheel

Go

Verified Radial Stress in Rotating Flywheel at given Radius

Go

Verified Tangential Stress in Rotating Flywheel at given Radius

Go

Verified Tensile Stress in Spokes of Rimmed Flywheel

Go

16 More Design of Flywheel Calculators

Go

Verified Bending Stress in Roller Pin of Forked End of Rocker Arm given Bending Moment

Go

Verified Diameter of Roller Pin of Forked End of Rocker Arm Considering Double Shear Failure of Pin

Go

Verified Diameter of Roller Pin of Forked End of Rocker Arm given Force at Roller Pin

Go

Verified Diameter of Roller Pin of Forked End of Rocker Arm given Outer Diameter of Eye of Roller Pin

Go

Verified Force on Roller Pin of Forked End of Rocker Arm

Go

Verified Force on Roller Pin of Forked End of Rocker Arm given Shear Stress in Roller Pin

Go

Verified Length of Roller Pin of Forked End of Rocker Arm

Go

Verified Length of Roller Pin of Forked End of Rocker Arm Considering Double Shear Failure of Pin

Go

Verified Length of Roller Pin of Forked End of Rocker Arm given Force at Roller Pin

Go

Verified Maximum Bending Moment in Roller Pin of Forked End of Rocker Arm

Go

Verified Shear Stress in Roller Pin of Forked End of Rocker Arm

Go

Verified Shear Stress in Roller Pin of Forked End of Rocker Arm given Force on Roller Pin

Go

10 More Design of Forked End Calculators

Go

Verified Angle between Two Arms of Rocker Arm

Go

Verified Bearing Pressure at Fulcrum Pin of Rocker Arm

Go

Verified Diameter of Fulcrum Pin of Rocker Arm Considering Double Shear Failure of Pin

Go

Verified Diameter of Fulcrum Pin of Rocker Arm given Length of Fulcrum Pin

Go

Verified Length of Fulcrum Pin of Rocker Arm considering Double Shear Failure of Pin

Go

Verified Reaction at Fulcrum Pin of Rocker Arm

Go

Verified Reaction at Fulcrum Pin of Rocker Arm for Equal Arm Lengths

Go

Verified Shear Stress in Fulcrum Pin of Rocker Arm given Reaction at Pin

Go

9 More Design of Fulcrum Pin Calculators

Go

Verified Bearing pressure in fulcrum pin of lever given reaction force and diameter of pin

Go

Verified Compressive stress in fulcrum pin of lever given reaction force, depth of lever arm

Go

Verified Diameter of fulcrum pin given compressive stress in pin

Go

Verified Diameter of fulcrum pin of lever given bending moment and effort force

Go

Verified Diameter of fulcrum pin of lever given reaction force and bearing pressure

Go

Verified Length of flucrum pin of lever given reaction force and bearing pressure

Go

Verified Length of fulcrum pin boss given compressive stress in pin

Go

Verified Maximum length of flucrum pin of lever given diameter of fulcrum pin

Go

Verified Bending Moment given Bending Stress in Hollow Shaft

Go

Verified Bending Stress in Hollow Shaft

Go

Verified Outer Diameter of Hollow Shaft given Bending Stress of Hollow Shaft

Go

Verified Torsional Shear Stress when Shaft is Subjected to Pure Torsional Moment

Go

19 More Design of Hollow Shaft Calculators

Go

Verified Polar Moment of Inertia of Hollow Circular Shaft

Go

Verified Shear Stress on Flat Key

Go

14 More Design of Machine Elements Calculators

Go

Verified Decrease in Outer Diameter of Cylinder given Total deformation in Pressure Vessel

Go

Verified Increase in Inner Diameter of Jacket given Total deformation of Pressure Vessel

Go

Verified Internal Diameter of Pressurized Cylinder

Go

Verified Maximum Load inside Pressurized Cylinder when Joint is on verge of opening

Go

Verified Thickness of Pressurized Cylinder

Go

Verified Total Deformation of Pressure Vessel given Increase in Inner Diameter of Jacket

Go

Created Diameter of rivet

Go

Created Diameter of rivet given efficiency of riveted joint

Go

Created Diameter of rivet(for dimension in cm)

Go

Created Efficiency of riveted joint given pitch of rivet

Go

Created Force transmitted across joints given number of rivets in small joint

Go

Created Least rivet value for shearing and bearing given number of rivets in small joint

Go

Created Number of rivets in small joint

Go

Created Pitch of rivets given efficiency of riveted joint and diameter of rivet

Go

Created Thickness of cover plate for butt joint with double cover plate

Go

Created Thickness of cover plate for butt joint with single cover plate

Go

Created Thickness of main plate given thickness of cover plate for butt joint with double cover plate

Go

Created Thickness of main plate given thickness of cover plate for butt joint with single cover plate

Go

Created Thickness of main plate(for dimension in cm)

Go

Created Thickness of main plate(for dimension in mm)

Go

Verified Bore Diameter of Bearing

Go

Verified Coefficient of Friction of Roller Contact Bearing

Go

Verified Friction Moment on Roller Contact Bearing

Go

Verified Load on Bearing given Moment on bearing

Go

Verified Median Life of Roller Contact Bearing

Go

Verified Nominal Life of Roller Contact Bearing

Go

Verified Number of Bearings required given Reliability

Go

Verified Reliability of Bearing

Go

Verified Reliability of Bearing given Number of Bearings

Go

Verified Reliability of Complete Bearing System

Go

Verified Speed of Rotation of Bearing

Go

Verified Train Wheel Diameter considering Bearing Life

Go

9 More Design of Rolling Contact Bearing Calculators

Go

Verified Angle of twist of hollow cylindrical rod in degrees

Go

Verified Angle of twist of solid cylindrical rod in degrees

Go

Verified Polar moment of inertia of shaft given shear stress and torsional moment

Go

Verified Torsional moment on shaft given shear stress

Go

5 More Design of Shaft for Torsional Moment Calculators

Go

Verified Bending Moment in horizantal plane of centre crankshaft below flywheel at TDC due to belt tension

Go

Verified Bending Moment in vertical plane of centre crankshaft below flywheel at TDC due to flywheel weight

Go

Verified Bending stress in centre crankshaft at TDC position below flywheel given shaft diameter

Go

Verified Diameter of part of centre crankshaft under flywheel at TDC position

Go

Verified Gap of Bearing 2 from Flywheel of centre crankshaft at TDC position

Go

Verified Gap of Bearing 3 from Flywheel of centre crankshaft at TDC position

Go

Verified Resultant Bending Moment in centre crankshaft at TDC position below flywheel

Go

Verified Resultant Bending Moment in centre crankshaft at TDC position below flywheel given shaft diameter

Go

Verified Torsional moment at central plane of centre crankshaft below flywheel at max torque

Go

5 More Design of Shaft Under Flywheel Calculators

Go

Verified Bending Moment in horizontal plane of side crankshaft at TDC position below flywheel due to flywheel

Go

Verified Bending Moment in vertical plane of side crankshaft at TDC position below flywheel due to flywheel

Go

Verified Diameter of part of side crankshaft under flywheel at TDC position

Go

Verified Resultant Bending Moment in side crankshaft at TDC position below flywheel

Go

Verified Resultant Bending Moment in side crankshaft at TDC position below flywheel given shaft diameter

Go

Verified Resultant Bending stress in side crankshaft at TDC position below flywheel given bending moment

Go

2 More Design of Shaft Under Flywheel Calculators

Go

Verified Distance between Front and Rear Wheel

Go

11 More Design of Superelevation Calculators

Go

Verified Compressive Force on Tappet of Rocker Arm of Engine Valve

Go

Verified Compressive Stress in Tappet of Rocker Arm of Engine Valve

Go

Verified Core Diameter of Tappet or Stud of Rocker Arm of Engine Valve

Go

Verified Depth of Circular End of Rocker Arm of Engine Valve

Go

Verified Nominal Diameter of Tappet or Stud of Rocker Arm of Engine Valve

Go

5 More Design of Tappet Calculators

Go

Verified Design Speed given Total Length of Valley Curve

Go

Verified Deviation Angle given Total Length of Valley Curve

Go

Verified Rate of Change of Acceleration given Total Length of Valley Curve

Go

Verified Total Length of Valley Curve

Go

8 More Design of Valley Curve Calculators

Go

Verified Diametral Quotient of Worm Gear

Go

6 More Design of Worm Gear Calculators

Go

Verified Efficiency of Machine given Mechanical Advantage and Velocity Ratio

Go

Verified Effort Required by Machine to Overcome Resistance to Get Work Done

Go

Verified Ideal Effort given Load and Velocity Ratio

Go

Verified Ideal Load given Velocity Ratio and Effort

Go

Verified Load Lifted given Effort and Mechanical Advantage

Go

Verified Mechanical Advantage given Load and Effort

Go

Verified Useful Work Output of Machine

Go

Verified Velocity Ratio given Distance Moved due to Effort and Distance Moved due to Load

Go

Verified Work Done by Effort

Go

1 More Design Parameters in Lifting Machines Calculators

Go

Created Angle of Twist with known Shear Strain at Outer Surface of Shaft

Go

Created Angle of Twist with known Shear Stress in Shaft

Go

Created Angle of Twist with known Shear Stress induced at Radius r from Center of Shaft

Go

Created Length of Shaft with known Shear Strain at Outer Surface of Shaft

Go

Created Length of Shaft with known Shear Stress induced at Radius r from Center of Shaft

Go

Created Length of Shaft with known Shear Stress induced at Surface of Shaft

Go

Created Modulus of Rigidity of material of Shaft using Shear Stress-induced at Surface of Shaft

Go

Created Modulus of Rigidity of Shaft if Shear Stress-induced at Radius 'r' from Center of Shaft

Go

Created Radius of Shaft if Shear Stress induced at Radius r from Center of Shaft

Go

Created Radius of Shaft using Shear Strain at Outer Surface of Shaft

Go

Created Radius of Shaft using Shear Stress induced at Surface of Shaft

Go

Created Shear Strain at Outer Surface of Circular Shaft

Go

Created Shear Stress at Surface of Shaft using Shear Stress-induced at Radius 'r' from Center of Shaft

Go

Created Shear Stress induced at Radius 'r' from Center of Shaft

Go

Created Shear Stress induced at Radius 'r' from Center of Shaft using Modulus of Rigidity

Go

Created Shear Stress induced at Surface of Shaft

Go

Created Value of Radius r using Shear Stress induced at Radius r from Center of Shaft

Go

Verified Diameter of Knuckle Pin given Bending Stress in Pin

Go

Verified Diameter of Pin of Knuckle Joint given Compressive Stress in Eye End Portion of Pin

Go

Verified Diameter of Pin of Knuckle Joint given Compressive Stress in Fork End Portion of Pin

Go

Verified Diameter of Pin of Knuckle Joint given Diameter of Pinhead

Go

Verified Diameter of Pin of Knuckle Joint given Load and Shear Stress in Pin

Go

Verified Diameter of Pin of Knuckle Joint given Shear Stress in Fork

Go

Verified Diameter of Pin of Knuckle Joint given Tensile Stress in Fork

Go

Verified Diameter of Pinhead of Knuckle Joint given Diameter of Pin

Go

Verified Length of Pin of Knuckle Joint in Contact with Eye End

Go

4 More Diameter of Pin of Knuckle joint Calculators

Go

Verified Inner Diameter of Engine Push Rod given Radius of Gyration

Go

Verified Maximum Inner Diameter of Engine Push Rod given Outer Diameter

Go

Verified Maximum Outer Diameter of Engine Push Rod given Inner Diameter

Go

Verified Minimum Inner Diameter of Engine Push Rod given Outer Diameter

Go

Verified Minimum Outer Diameter of Engine Push Rod given Inner Diameter

Go

Verified Outer Diameter of Engine Push Rod given Radius of Gyration

Go

Created Diameter of rivet given crushing strength for double rivet

Go

Created Diameter of rivet given crushing strength for 'n' number of rivets

Go

Created Diameter of rivet given crushing strength for single rivet

Go

Created Diameter of rivet given crushing strength for triple-rivet

Go

Created Diameter of rivet given shearing strength if rivet is in double shear

Go

Created Diameter of rivet given shearing strength if rivet is in single shear

Go

Created Diameter of rivet given tearing strength of rivet

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Verified Diameter of Rod of Cotter Joint given Socket Collar Diameter

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Verified Diameter of Rod of Cotter Joint given Spigot Collar Diameter

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Verified Diameter of Rod of Cotter Joint given Thickness of Cotter

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Verified Diameter of Rod of Cotter Joint given Thickness of Spigot Collar

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1 More Diameter of Rod of Cotter Joint Calculators

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Verified Diameter of Rod of Knuckle Joint given its Enlarged Diameter near Joint

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Verified Diameter of Rod of Knuckle Joint given Tensile Stress in Rod

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Verified Enlarged Diameter of Rod of Knuckle Joint near Joint

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Verified Rod Diameter of Knuckle Joint given Thickness of Eye

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Verified Rod Diameter of Knuckle Joint given Thickness of Fork Eye

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Verified Diameter of Socket Collar of Cotter Joint given Bending Stress in Cotter

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Verified Diameter of Socket Collar of Cotter Joint given Compressive Stress

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Verified Diameter of socket collar of cotter joint given shear stress in socket

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Verified Inside Diameter of Socket of Cotter Joint given Shear Stress in Socket

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1 More Diameter of Socket Collar Calculators

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Verified Diameter of Spigot of Cotter Joint given Bending Stress in Cotter

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Verified Diameter of Spigot of Cotter Joint given Compressive Stress

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Verified Diameter of Spigot of Cotter Joint given Shear Stress in Spigot

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3 More Diameter of Spigot and Spigot Collar Calculators

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Created Diameter of Spring Wire given Deflection of Spring

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Created Diameter of Spring Wire given Maximum Shear Stress induced in Wire

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Created Diameter of Spring Wire given Stiffness of Helical Spring

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Created Diameter of Spring Wire given Strain Energy Stored by Spring

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Created Diameter of Spring Wire given Twisting Moment

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Verified Diameter of Wire of Engine Valve Spring

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Verified Diameter of Wire of Engine Valve Spring given Maximum Compression in Spring

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Verified Diameter of Wire of Engine Valve Spring given Number of Active Turns of Spring

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Verified Spring Index of Engine Valve Spring given Shear Stress, Maximum Force and Wire Diameter

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Verified Wahl Factor for Engine Valve Spring given Mean Coil Diameter and Wire Diameter

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Verified Wahl Factor for Engine Valve Spring given Spring Index

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3 More Diameter of Spring Wire Calculators

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Created Diameter of wire given bursting force due to fluid pressure

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Created Diameter of wire given compressive circumferential stress exerted by wire

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Created Diameter of wire given initial tensile force and length of wire

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Created Diameter of wire given initial tensile force in wire

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Created Diameter of wire given number of turns of wire in length L

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Created Diameter of wire given resisting force of wire per cm length

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Created Diameter of wire given resisting force on wire

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Verified Differential Voltage Gain in MOS Differential Amplifier

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Verified Input Offset Voltage of MOS Differential Amplifier

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Verified Input Offset Voltage of MOS Differential Amplifier when Aspect Ratio Mismatches

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6 More Differential Configuration Calculators

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Verified Bingham Number

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Verified Buoyant force given grashof number

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Verified Eckert Number

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Verified Heat diffusivity given Lewis number

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Verified Modified Rayleigh number given Bingham number

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Verified Viscous force given grashofs number

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14 More Dimensionless groups Calculators

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Verified Grashof Number

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10 More Dimensionless Numbers Calculators

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Verified Coefficient of Friction in Terms of Coefficient of friction Variable

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Verified Coefficient of Friction Variable of Bearing in Terms of Coefficient of Friction

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Verified Flow Ratio Variable in Terms of Outflow of Lubricant

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Verified Flow Variable in Terms of Flow of Lubricant in Clearance Space of Journal

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Verified Load Coefficient in Terms of Load Acting on Bearing

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Verified Radial Clearance in Terms of Coefficient of Friction Variable of Bearing

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Verified Radius of Journal in Terms of Coefficient of Friction Variable

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Verified Sommerfeld Number of Bearing

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Verified Angle between arms of lever given effort, load and net reaction at fulcrum

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Verified Depth of lever arm given width

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Verified Length of major axis for elliptical cross sectioned lever given minor axis

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Verified Length of minor axis for elliptical cross sectioned lever given major axis

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Verified Outside diameter of boss in lever

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Verified Width of lever arm given depth

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Verified Direct Count

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Verified Tex Count

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3 More Direct Count System Calculators

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Verified Modulus of Rigidity using Young's Modulus and Poisson's Ratio

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Verified Poisson's ratio given tensile strain due to compressive stress in diagonal BD

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Verified Poisson's Ratio using Modulus of Rigidity

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Verified Shear Strain in Diagonal given Tensile Strain for Square Block

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Verified Tensile strain in diagonal BD of square block ABCD due to compressive stress

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Verified Tensile Strain in Diagonal given Shear Strain for Square Block

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Verified Tensile Strain in Diagonal of Square Block due to Tensile Stress

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Verified Total Compressive Strain in Diagonal AC of Square Block ABCD

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Verified Total tensile strain in diagonal BD of square block ABCD given modulus of rigidity

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Verified Total Tensile Strain in Diagonal of Square Block

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Verified Young's Modulus using Modulus of Rigidity

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Verified Rate of flow of liquid into air vessel

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Verified Rate of Flow of Liquid into Air Vessel given Stroke Length

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Verified Weight of Water delivered per second given Density and Discharge

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8 More Discharge Calculators

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Verified Discharge Current

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Verified Discharge Voltage

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Verified Resistance of Discharging Circuit Discharge Voltage

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Verified Capacitance of Circuit from Resistance of Discharging Circuit

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Verified Discharging Voltage

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Verified Resistance of Discharging Circuit from Capacitance

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Verified Time Elapsed

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Verified Voltage of Charging Circuit

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Verified Distance from Start given Restoring Force and Constant K

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Verified Distance Traveled given Velocity

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Verified Total Distance Traveled given Velocity and Angular Frequency

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Verified Distortion Strain Energy

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Verified Distortion Strain Energy for Yielding

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Verified Shear Yield Strength by Maximum Distortion Energy Theorem

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Verified Tensile Yield Strength by Distortion Energy Theorem

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Verified Tensile Yield Strength by Distortion Energy Theorem Considering Factor of Safety

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Verified Tensile Yield Strength for Biaxial Stress by Distortion Energy Theorem Considering Factor of Safety

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7 More Distortion Energy Theory Calculators

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Verified Efficiency of draft tube

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Verified Head loss in draft tube given efficiency

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Verified Velocity of water at inlet of draft tube given draft tube efficiency

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Verified Velocity of water at outlet of draft tube given draft tube efficiency

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Verified Induced Drag Coefficient

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Verified Induced Drag Coefficient given Total Drag Coefficient

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Verified Profile Drag Coefficient

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Verified Profile Drag Coefficient given Total Drag Coefficient

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Verified Total Drag Coefficient for Subsonic Finite Wing

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Verified Buoyant force acting on spherical ball

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Verified Drag Force for body moving in Fluid

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Verified Power Required to Keep Flat Plate in Motion

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4 More Drag Force on Body Calculators

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Verified Blank Size for Drawing Operation

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Verified Drawing Force for Cylindrical Shells

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3 More Drawing Operation Calculators

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Verified Axial Force of Multiplate Clutch using Uniform Wear Theory

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Verified Effective Gear Ratio

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Verified Final Drive Ratio

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11 More Driveline Calculators

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Verified Torque Transmitted by n Friction Surfaces

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Verified Torque Transmitted by n Friction Surfaces using Uniform Wear Theory

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1 More Driveline Torque Calculators

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Verified Dynamic Load Capacity for Ball Bearing

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Verified Dynamic Load Capacity for Bearing given Rated Bearing Life

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Verified Dynamic Load Capacity for Roller Bearing

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Verified Equivalent Dynamic Load for Ball Bearing

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Verified Equivalent Dynamic Load for Bearing given Rated Bearing Life

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Verified Equivalent Dynamic Load for Roller Bearing

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1 More Dynamic Load Calculators

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Verified Dynamic Loss Coefficient given Dynamic Pressure Loss

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Verified Dynamic Loss Coefficient given Equivalent Additional Length

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Verified Dynamic Pressure Loss

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Verified Pressure Loss at Discharge or Exit

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Verified Pressure Loss at Suction

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Verified Pressure Loss Coefficient at Inlet of Duct

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Verified Pressure Loss Coefficient at Outlet of Duct

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Verified Pressure Loss due to Gradual Contraction given Pressure Loss Coefficient at Section 1

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Verified Pressure Loss due to Gradual Contraction given Velocity of Air at Point 2

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Verified Pressure Loss due to Sudden Contraction given Velocity of Air at Point 1

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Verified Pressure Loss due to Sudden Contraction given Velocity of Air at point 2

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Verified Pressure Loss due to Sudden Enlargement

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Verified Angle of banking

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4 More Dynamics Calculators

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Created Constant for Particular Shaft for Torsion Dynamometer

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Created Distance Moved in One Revolution by Rope Brake Dynamometer

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Created Load on Brake for Rope Brake Dynamometer

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Created Tangential Effort for Epicyclic-Train Dynamometer

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Created Tension in Slack Side of Belt for Belt Transmission Dynamometer

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Created Tension in Tight Side of Belt for Belt Transmission Dynamometer

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Created Torsion Equation for Torsion Dynamometer

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Created Torsion Equation for Torsion Dynamometer using Modulus of Rigidity

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Verified Imaginary Force at Center of Gravity of Bolted Joint given Primary Shear Force

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Verified Number of Bolts given Primary Shear Force

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Verified Primary Shear Force of Eccentrically Loaded Bolted Connection

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Verified Eccentricity of Bearing in Terms of Minimum Film Thickness

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Verified Eccentricity of Bearing in Terms of Radial Clearance and Eccentricity

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Verified Eccentricity Ratio in Terms of Minimum Film Thickness of Bearing

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Verified Eccentricity Ratio of Bearing in Terms of Minimum Film Thickness Variable

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Verified Eccentricity Ratio of Bearing in Terms of Radial Clearance and Eccentricity

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Created Angular Velocity of Element

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Created Angular Velocity of Free End using Kinetic Energy of Constraint

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Created Kinetic Energy Possessed by Element

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Created Mass Moment of Inertia of Element

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Created Natural Frequency of Torsional Vibration due to Effect of Inertia of Constraint

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Created Torsional Stiffness of Shaft due to Effect of Constraint on Torsional Vibrations

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Created Total Kinetic Energy of Constraint

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Created Total Mass Moment of Inertia of Constraint given Kinetic Energy of Constraint

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Created Diameter of cylindrical shell given change in length of cylindrical shell

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Created Diameter of thin cylindrical shell given volumetric strain

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Created Diameter of thin cylindrical strain given volumetric strain

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Created Hoop stress given circumferential strain

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Created Hoop stress in thin cylindrical vessel given Longitudinal strain

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Created Internal diameter of thin cylindrical vessel given circumferential strain

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Created Internal diameter of thin cylindrical vessel given longitudinal strain

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Created Internal fluid pressure given change in length of cylindrical shell

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Created Internal fluid pressure given circumferential strain

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Created Internal fluid pressure in shell given volumetric strain

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Created Internal fluid pressure in thin cylindrical vessel given change in diameter

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Created Internal fluid pressure in thin cylindrical vessel given longitudinal strain

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Created Length of cylindrical shell given change in length of cylindrical shell

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Created Length of cylindrical shell given change in volume of cylindrical shell

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Created Length of thin cylindrical strain given volumetric strain

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Created Longitudinal stress given circumferential strain

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Created Longitudinal stress in thin cylindrical vessel given Longitudinal strain

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Created Original circumference of thin cylindrical vessel given circumferential strain

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Created Original diameter of thin cylindrical vessel given circumferential strain

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Created Original diameter of vessel given change in diameter

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Created Original length of vessel given longitudinal strain

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Created Original volume of cylindrical shell given volumetric strain

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Created Volume of thin cylindrical shell given circumferential and longitudinal strain

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Verified Effective Angle of Attack of Finite Wing

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Verified Geometric Angle of Attack given Effective Angle of Attack

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Verified Induced Angle of Attack given Effective Angle of Attack

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Verified Dynamic load on Gear

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Verified Tolerance factor of Gear

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11 More Effective Load on Gear Tooth Calculators

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Verified Effective thermal conductivity for annular space between concentric cylinders

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Verified Effective thermal conductivity given Prandtl number

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Verified Heat transfer per unit length for annular space between concentric cylinders

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5 More Effective Thermal Conductivity and Heat Transfer Calculators

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Verified Effectiveness of double pipe counter flow heat exchanger given C equal to 1

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Verified Effectiveness when mc-cc is minimum value

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Verified Effectiveness when mhch is minimum value

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9 More Effectiveness Calculators

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Verified Efficiency of Cooling Coil

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Verified Efficiency of Cooling Coil given By-pass Factor

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Verified Efficiency of Heating Coil

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Verified Efficiency of Heating Coil given By-pass Factor

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Created Efficiency of circumferential joint given longitudinal stress

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Created Efficiency of longitudinal joint given hoop stress

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Created Hoop stress given efficiency of longitudinal joint

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Created Internal diameter of vessel given hoop stress and efficiency of longitudinal joint

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Created Internal diameter of vessel given longitudinal stress and efficiency of circumferential joint

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Created Internal fluid pressure given longitudinal stress and efficiency of circumferential joint

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Created Internal fluid pressure in vessel given hoop stress and efficiency of longitudinal joint

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Created Longitudinal stress given efficiency of circumferential joint

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Created Thickness of vessel given hoop stress and efficiency of longitudinal joint

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Created Thickness of vessel given longitudinal stress and efficiency of circumferential joint

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Created Effort of Porter Governor if Angle Made by Upper and Lower Arms are Equal

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Created Effort of Porter Governor if Angle Made by Upper and Lower Arms are Not Equal

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Created Force in Arm of Porter Governor given Centrifugal Force on Ball

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Created Force in Arm of Porter Governor given Force in Link

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Created Force in Arm of Porter Governor given Mass of Central Load and Ball

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Created Force in Arm of Porter Governor given Weight of Central Load and Ball

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Created Force in Link of Porter Governor given Mass of Central Load

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Created Force in Link of Porter Governor given Weight of Central Load

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Created Radial Force on Each Ball in Porter Governor

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Verified Effort Force Applied on Lever given Bending Moment

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Verified Reaction Force at Fulcrum of Lever given Bearing Pressure

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Verified Reaction Force at Fulcrum of Lever given Effort, Load and Contained Angle

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Verified Reaction Force at Fulcrum of Right Angled Lever

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6 More Effort, Load and Reaction on Lever Calculators

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Verified Bulk Modulus given Shear Modulus and Young's Modulus

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Verified Shear Modulus given Young's Modulus and Bulk Modulus

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Verified Youngs Modulus given Shear Modulus and Bulk Modulus

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Verified Diameter of Bolt given Frictional Force exerted by Soft packing on Reciprocating rod

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Verified Fluid pressure by soft packing exerted by frictional force on reciprocating rod

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Verified Fluid Pressure given Friction Resistance

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Verified Fluid Pressure given Torsional Resistance

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Verified Friction resistance

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Verified Frictional force exerted by soft packing on reciprocating rod

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Verified Seal resistance

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Verified Torsional Resistance given Fluid Pressure

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Verified Torsional resistance in rotary motion friction

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Verified Area of Body given Stress

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Verified Change in Length given Longitudinal Stress

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Verified Change in Volume of Body given Volumetric Strain

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Verified Displacement of Upper Surface

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Verified Normal Stress or Longitudinal Stress

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Verified Original Length given Longitudinal Stress

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Verified Original Volume of Body given Volumetric Strain

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Verified Volume Strain

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Verified Young's Modulus of Elasticity

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Verified Accelaration given Constant K and Distance Traveled

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Verified Mass of Body given Distance Traveled and Constant K

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Verified Mass of Particle given Angular Frequency

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Verified Perpendicular Distance between Two Surfaces

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Verified Restoring Force given Stress

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Verified Electric Current given Drift Velocity

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Verified Electric Field due to Line Charge

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Verified Electric Force by Coulomb's Law

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10 More Electrostatics Calculators

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Verified Aspect Ratio given Induced Angle of Attack

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Verified Aspect Ratio given Induced Drag Coefficient

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Verified Circulation at given Distance along Wingspan

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Verified Circulation at Origin given Downwash

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Verified Circulation at Origin given Induced Angle of Attack

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Verified Circulation at Origin given Lift of Wing

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Verified Circulation at Origin in Elliptical Lift Distribution

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Verified Coefficient of Lift given Circulation at Origin

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Verified Coefficient of Lift given Induced Angle of Attack

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Verified Coefficient of Lift given Induced Drag Coefficient

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Verified Downwash in Elliptical Lift Distribution

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Verified Freestream Velocity given Circulation at Origin

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Verified Freestream Velocity given Induced Angle of Attack

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Verified Induced Angle of Attack given Aspect Ratio

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Verified Induced Angle of Attack given Circulation at Origin

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Verified Induced Angle of Attack given Coefficient of Lift

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Verified Induced Angle of Attack given Downwash

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Verified Induced Drag Coefficient given Aspect Ratio

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Verified Lift at given Distance along Wingspan

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Verified Lift of Wing given Circulation at Origin

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Verified Specific Energy of Elliptic Orbit given Angular Momentum

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Verified Specific Energy of Elliptic Orbit given Semi Major Axis

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Verified Time Period for One Complete Revolution given Angular Momentum

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Verified Time Period of Elliptical Orbit given Angular Momentum

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12 More Elliptical Orbits Calculators

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Verified Bar's total elongation if weight given per unit volume of bar

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Verified Elongation of element

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Verified Length of Bar given Total Elongation of Bar

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Verified Length of Bar using Total Elongation and Weight per unit volume of bar

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Verified Modulus of Elasticity given Total Elongation of Bar

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Verified Strain in Element

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Verified Stress on element of rod

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Verified Total elongation of bar

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Verified Weight of bar for length x

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Verified Weight of Bar given Total Elongation of Bar

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Verified Maximum Thickness of Cylinder Flange given Nominal Diameter of Stud

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Verified Maximum Thickness of Cylinder Flange given Thickness of Cylinder Wall

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Verified Maximum Thickness of Dry Liner

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Verified Maximum Thickness of Water Jacket Wall

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Verified Minimum Thickness of Cylinder Flange given Nominal Diameter of Stud

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Verified Minimum Thickness of Cylinder Flange given Thickness of Cylinder Wall

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Verified Minimum Thickness of Dry Liner

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Verified Minimum Thickness of Water Jacket Wall

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Verified Thickness of Engine Cylinder Wall given Cylinder Inner Diameter

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Verified Water Space between Outer Cylinder Wall and Inner Jacket Wall

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Verified Amplitude given Position

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Verified Constant K given Angular Frequency

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Verified Constant K given Restoring Force

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Verified Endurance Limit for Axial Loading

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Verified Endurance Limit given Endurance Limit for Axial Loading

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Verified Endurance Limit of Rotating Beam Specimen

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Verified Endurance Limit of Specimen

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Verified Fatigue Stress Concentration Factor given Modifying Factor

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Verified Modifying Factor for Fluctuating Load given Fatigue Stress Concentration Factor

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Verified Modifying Factor to Account for Stress Concentration

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Verified Reliability Factor for Fluctuating Load

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Verified Size Factor for Fluctuating Load

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Verified Surface Finish Factor of Specimen

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5 More Endurance Limit Approximate Estimation in Design Calculators

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Verified Energy Density of Magnetic Field

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2 More Energy Calculators

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Verified Depth of Crater

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Verified Energy per Spark from Depth of Crater

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3 More Energy delivered per spark Calculators

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Verified Engine rpm

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7 More Engine Calculators

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Verified Brake Power given Mean Effective Pressure

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Verified Brake Power given Mechanical Efficiency

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Verified Brake specific fuel consumption

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Verified Brake Thermal Efficiency given Brake Power

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Verified Friction Power

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Verified Indicated Power given Mechanical Efficiency

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Verified Indicated specific fuel consumption

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Verified Indicated Thermal Efficiency given Indicated Power

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Verified Indicated Thermal Efficiency given Relative Efficiency

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Verified Inlet-Valve Mach Index

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Verified Mechanical Efficiency of IC engine

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Verified Relative Efficiency

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Verified Specific Power Output

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List of Calculators by Anshika Arya