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Calculators Created by Anshika Arya
Anshika Arya
National Institute Of Technology
(NIT)
,
Hamirpur
1977
Formulas Created
2679
Formulas Verified
710
Across Categories
List of Calculators by Anshika Arya
Following is a combined list of all the calculators that have been created and verified by Anshika Arya. Anshika Arya has created 1977 and verified 2679 calculators across 710 different categories till date.
CS Amplifier
(10)
Verified
3 dB frequency of CS amplifier
Go
Verified
3 dB frequency of CS amplifier without dominant poles
Go
Verified
3-dB frequency from Method of Short-Circuit Time Constants
Go
Verified
Frequency of zero transmission of CS Amplifier
Go
Verified
Mid-band gain of CS amplifier
Go
Verified
Overall low frequency gain function of amplifier
Go
Verified
Pole frequency of bypass capacitor in CS Amplifier
Go
Verified
Pole frequency of CS Amplifier
Go
Verified
Signal voltage of CS amplifier
Go
Verified
Transmission zero on negative real axis of s plane
Go
High-Frequency Response of Amplifiers
(15)
Verified
3 dB frequency of CE amplifier
Go
Verified
3-dB frequency given time constant
Go
Verified
Collector base junction resistance of CE amplifier
Go
Verified
Drain voltage through method of Open-Circuit Time Constants to CS Amplifier
Go
Verified
Effective high frequency time constant of amplifier
Go
Verified
Effective high frequency time constant of CE amplifier
Go
Verified
Effective high-frequency time constant
Go
Verified
High frequency time constant of amplifier
Go
Verified
Open circuit time constant of amplifier
Go
Verified
Resistance between gate and drain in open circuit time constants method of CS amplifier
Go
Verified
Resistance between gate and drain in open-circuit time-constants method
Go
Verified
Test current in open circuit time constants method of CS amplifier
Go
Verified
Test current in open-circuit time-constants method
Go
Verified
Upper 3-dB frequency given open-circuit time constant
Go
Verified
Voltage between gate and source through method of Open-Circuit Time Constants to CS Amplifier
Go
4 More High-Frequency Response of Amplifiers Calculators
Go
High-Frequency Response of MOS Cascode Amplifier
(1)
Verified
Signal Current in Base
Go
9 More High-Frequency Response of MOS Cascode Amplifier Calculators
Go
Values of load for the various types of beams and under various load conditions.
(8)
Created
Eccentric Point Load for Fixed Beam
Go
Created
Eccentric Point Load for Simply Supported Beam
Go
Created
Value of load for Cantilever beam with point load at free end
Go
Created
Value of load for Cantilever beam with uniformly distributed load
Go
Created
Value of load for fixed beam with central point load
Go
Created
Value of load for fixed beam with uniformly distributed load
Go
Created
Value of load for simply supported beam with central point load
Go
Created
Value of load for simply supported beam with uniformly distributed load
Go
2 Wattmeter Method
(2)
Verified
Power in Wattmeter 1
Go
Verified
Power in Wattmeter 2
Go
1 More 2 Wattmeter Method Calculators
Go
AC Potentiometer
(1)
Verified
Phase Angle
Go
1 More AC Potentiometer Calculators
Go
Acceleration Of The Follower
(20)
Created
Acceleration of follower after time t for cycloidal motion
Go
Created
Acceleration of follower for circular arc cam if there's contact on circular flank
Go
Created
Acceleration of follower for roller follower tangent cam, there's contact with straight flanks
Go
Created
Acceleration of follower of roller follower tangent cam, there's contact with nose
Go
Created
Centripetal acceleration of point P on circumference
Go
Created
Centripetal acceleration of point P on circumference when follower moves with SHM
Go
Created
Max acceleration of follower during outstroke if outstroke velocity is known(uniform acceleration)
Go
Created
Max acceleration of follower during outstroke if stroke of follower is known(uniform acceleration)
Go
Created
Max acceleration of follower during return stroke if follower speed is known(uniform acceleration)
Go
Created
Max acceleration of follower during return stroke if follower stroke is known(uniform acceleration)
Go
Created
Max acceleration of follower for tangent cam with roller follower
Go
Created
Maximum Acceleration of Follower during Outstroke for Cycloidal Motion
Go
Created
Maximum acceleration of follower during return stroke for Cycloidal motion
Go
Created
Maximum Acceleration of Follower for Circular Arc Cam Contacting with Circular Flank
Go
Created
Maximum acceleration of follower on outstroke when follower moves with SHM
Go
Created
Maximum acceleration of follower on return stroke when follower moves with SHM
Go
Created
Maximum uniform acceleration of follower during outstroke
Go
Created
Maximum uniform acceleration of follower during return stroke
Go
Created
Min acceleration of follower for tangent cam with roller follower
Go
Created
Minimum Acceleration of Follower for Circular Arc Cam Contacting with Circular Flank
Go
Acme Thread
(1)
Verified
Torque Required in Lifting Load with Acme Threaded Power Screw
Go
17 More Acme Thread Calculators
Go
Addendum Circle Diameter
(1)
Verified
Addendum Circle Diameter of Large Size Gear
Go
4 More Addendum Circle Diameter Calculators
Go
Aerodynamic Drag and Its Reduction
(1)
Verified
Lateral plane span given aspect ratio
Go
40 More Aerodynamic Drag and Its Reduction Calculators
Go
Aerodynamics
(2)
Verified
Disk Loading
Go
Verified
Orbital Period
Go
9 More Aerodynamics Calculators
Go
Aircraft Endurance
(1)
Verified
Tip Speed Ratio with Blade Number
Go
3 More Aircraft Endurance Calculators
Go
Aircraft Preliminary Design
(1)
Verified
Winglet friction coefficient
Go
Aircraft Preliminary Weight Built Up
(16)
Verified
Crew Weight given Fuel and Empty Weight Fraction
Go
Verified
Crew Weight given Takeoff Weight
Go
Verified
Empty Weight given Empty Weight Fraction
Go
Verified
Empty Weight given Takeoff Weight
Go
Verified
Fuel Fraction given Takeoff Weight and Empty Weight Fraction
Go
Verified
Fuel Weight given Fuel Fraction
Go
Verified
Fuel Weight given Takeoff Weight
Go
Verified
Optimum Range for Jet Aircraft in Cruising Phase
Go
Verified
Optimum Range for Prop-Driven Aircraft in Cruising Phase
Go
Verified
Payload Weight given Fuel and Empty Weight Fractions
Go
Verified
Payload Weight given Takeoff Weight
Go
Verified
Preliminary Endurance for Jet Aircraft
Go
Verified
Preliminary Take Off Weight Built-up for manned aircraft
Go
Verified
Preliminary Take off Weight Built-up for Manned Aircraft given Fuel and Empty Weight Fraction
Go
Verified
Takeoff Weight given Empty Weight Fraction
Go
Verified
Takeoff Weight given Fuel Fraction
Go
5 More Aircraft Preliminary Weight Built Up Calculators
Go
Air-Standard Cycles
(7)
Verified
Air standard efficiency for Diesel engines
Go
Verified
Air standard efficiency for Petrol engines
Go
Verified
Air Standard Efficiency given Relative Efficiency
Go
Verified
Mean Effective Pressure in Diesel Cycle
Go
Verified
Work Output for Diesel Cycle
Go
Verified
Work Output for Dual Cycle
Go
Verified
Work Output for Otto Cycle
Go
4 More Air-Standard Cycles Calculators
Go
Allowable Stress
(9)
Created
Allowable crushing stress of rivet material given crushing strength for double rivet
Go
Created
Allowable crushing stress of rivet material given crushing strength for 'n' number of rivets
Go
Created
Allowable crushing stress of rivet material given crushing strength for single rivet
Go
Created
Allowable crushing stress of rivet material given crushing strength for triple rivet
Go
Created
Allowable shear stress of rivet material given shearing strength if rivet is in double shear
Go
Created
Allowable shear stress of rivet material given shearing strength if rivet is in single shear
Go
Created
Allowable tensile stress in plate given strength of solid plate per pitch length
Go
Created
Allowable tensile stress in plate given tearing strength of rivet
Go
Created
Allowable tensile stress in plates given efficiency of riveted joint
Go
Amplification factor
(7)
Verified
Closed loop voltage gain in ideal case of Feedback Voltage Amplifiers
Go
Verified
Feedback voltage of feedback amplifier
Go
Verified
Input current of feedback amplifier given amount of feedback
Go
Verified
Input resistance of feedback amplifier
Go
Verified
Input voltage of feedback amplifier
Go
Verified
Input voltage of Feedback Voltage Amplifiers
Go
Verified
Output resistance of feedback amplifier
Go
7 More Amplification factor Calculators
Go
Amplification Factor
(1)
Verified
Signal Current in Emitter given Input Signal
Go
13 More Amplification Factor Calculators
Go
Amplification Factor
(9)
Verified
Current transfer ratio of IC Amplifier
Go
Verified
Current transfer ratio of mirror with base current compensation
Go
Verified
Input resistance in small-signal operation of current mirrors
Go
Verified
Output current given reference current
Go
Verified
Output current of BJT mirror
Go
Verified
Output resistance of simple current BJT
Go
Verified
Output resistance of simple current BJT given early voltage
Go
Verified
Reference current of BJT current mirror
Go
Verified
Voltage gain of small-signal operation of current mirrors given aspect ratio
Go
4 More Amplification Factor Calculators
Go
Amplification Factor
(13)
Verified
3-dB frequency with no dominant pole
Go
Verified
Closed-loop gain as function of ideal value
Go
Verified
Closed-loop gain when AB is greater than 1
Go
Verified
Feedback signal of feedback amplifier
Go
Verified
Feedback signal of feedback amplifier given output signal
Go
Verified
Gain with-feedback of feedback amplifier
Go
Verified
Gain-with-feedback when AB is greater than 1
Go
Verified
Input signal to basic amplifier
Go
Verified
Returned Signal
Go
Verified
Signal voltage of source follower
Go
Verified
Signal voltage of source follower given capacitance
Go
Verified
Test Signal
Go
Verified
Transition frequency
Go
3 More Amplification Factor Calculators
Go
Analysis of Bar of Uniform Strength
(2)
Verified
Area of lower end of bar
Go
Verified
Area of upper end of bar
Go
Analysis of Compound Weld
(14)
Created
Allowable tensile stress given load carried by single fillet lap weld
Go
Created
Allowable tensile stress given total load carried by plates in compound weld
Go
Created
Length of Parallel Fillet Weld given Load Carried by Parallel Fillet Weld
Go
Created
Length of Parallel Fillet Weld given Total Load Carried by Plates in Compound Weld
Go
Created
Length of single fillet lap weld given load carried by single fillet lap weld
Go
Created
Length of single fillet lap weld given total load carried by plates in compound weld
Go
Created
Load carried by parallel fillet weld
Go
Created
Load carried by single fillet lap weld
Go
Created
Maximum shear stress given load carried by parallel fillet weld
Go
Created
Maximum shear stress given total load carried by plates in compound weld
Go
Created
Thickness of plates given load carried by parallel fillet weld
Go
Created
Thickness of plates given load carried by single fillet lap weld
Go
Created
Thickness of plates given total load carried by plates in compound weld
Go
Created
Total load carried by plates in compound weld
Go
Analysis of Stresses
(4)
Verified
Maximum principal stress
Go
Verified
Minimum principal stress
Go
Verified
Shear stress on inclined plane
Go
Verified
Stress on inclined plane
Go
Analysis of Unsymmetrical Welded Sections which are Loaded Axially
(20)
Created
Area of unsymmetrical weld
Go
Created
Area of unsymmetrical weld given throat thickness
Go
Created
Area of weld given axial load on weld
Go
Created
Axial load on angle
Go
Created
Axial load on angle given resistance of bottom and top weld
Go
Created
Axial load on weld
Go
Created
Axial load on weld given shear stress
Go
Created
Shear stress given axial load on weld
Go
Created
Shear stress given axial load on welded connection
Go
Created
Thickness of plate given area of unsymmetrical weld
Go
Created
Thickness of plate given axial load on weld
Go
Created
Throat thickness given area of unsymmetrical weld
Go
Created
Total length of weld given area of unsymmetrical weld
Go
Created
Total length of weld given length of bottom weld
Go
Created
Total length of weld given length of top and bottom weld
Go
Created
Total length of weld given length of top weld
Go
Created
Total length of weld given resistance of bottom weld
Go
Created
Total length of weld given resistance of top weld
Go
Created
Total resistance given resistance of bottom weld
Go
Created
Total resistance given resistance of top weld
Go
Angular Contact Bearing
(9)
Verified
Axial Load for Back to Back Bearings when Fa by Fr is greater than 1.14
Go
Verified
Axial Load for Back to Back Bearings when Fa by Fr is less than or equal to 1.14
Go
Verified
Axial Load for Singly Mounted Bearings when Fa by Fr is greater than 1.14
Go
Verified
Equivalent Dynamic Load for Back to Back Bearings when Fa by Fr is greater than 1.14
Go
Verified
Equivalent Dynamic Load for Back to Back Bearings when Fa by Fr is less than or equal to 1.14
Go
Verified
Equivalent Dynamic Load for Singly Mounted Bearings when Fa by Fr is greater than 1.14
Go
Verified
Radial Load for Back to Back Bearings when Fa by Fr greater than 1.14
Go
Verified
Radial Load for Back to Back Bearings when Fa by Fr less than or equal to 1.14
Go
Verified
Radial Load for Singly Mounted Bearings when Fa by Fr is greater than 1.14
Go
Angular Frequency
(3)
Verified
Angular frequency given constant K and mass
Go
Verified
Angular frequency given velocity and distance A
Go
Verified
Angular frequency of shm
Go
Angular Velocity Of Disc
(9)
Created
Angular Velocity of disc given Circumferential stress at center of solid disc
Go
Created
Angular velocity of disc given Circumferential stress in solid disc
Go
Created
Angular velocity of disc given Constant at boundary condition for circular disc
Go
Created
Angular velocity of disc given maximum radial stress
Go
Created
Angular velocity of disc given Radial stress at center of solid disc
Go
Created
Angular Velocity of disc given Radial stress in solid disc
Go
Created
Angular velocity of disc given Radial stress in solid disc and Outer radius
Go
Created
Disc's Angular velocity given Circumferential stress and Outer radius
Go
Created
Disc's angular velocity given maximum circumferential stress in solid disc
Go
Anti Geometry of Independent Suspension
(17)
Verified
Angle between IC and ground
Go
Verified
Camber change rate
Go
Verified
Front view swing arm
Go
Verified
Height of centre of gravity from road surface from percentage anti dive
Go
Verified
Height of centre of gravity from road surface from percentage anti lift
Go
Verified
Percent anti squat
Go
Verified
Percentage anti dive on front
Go
Verified
Percentage anti lift
Go
Verified
Percentage front braking given percentage anti dive
Go
Verified
Percentage rear braking given percentage anti lift
Go
Verified
Roll camber
Go
Verified
Side view swing arm height given percentage anti dive
Go
Verified
Side view swing arm height given percentage anti lift
Go
Verified
Side view swing arm length given percentage anti dive
Go
Verified
Side view swing arm length given percentage anti lift
Go
Verified
Wheelbase of Vehicle from Percentage Anti Dive
Go
Verified
Wheelbase of Vehicle from Percentage Anti Lift
Go
Applications
(1)
Verified
Beale number
Go
12 More Applications Calculators
Go
Area of Fillet Weld
(8)
Created
Area of Double Fillet Weld given Tensile Force
Go
Created
Area of fillet weld given thickness of plate for single fillet lap joint
Go
Created
Area of fillet weld given throat thickness for double fillet lap joint
Go
Created
Area of fillet weld given throat thickness for single fillet lap joint
Go
Created
Area of fillet weld in given thickness of plate for double fillet lap joint
Go
Created
Area of parallel fillet weld given thickness of plate
Go
Created
Area of parallel fillet weld given throat thickness
Go
Created
Area of Single Fillet Weld given Tensile Force
Go
Area of Triangular Prism
(1)
Created
Total Surface Area of Triangular Prism given base Area
Go
7 More Area of Triangular Prism Calculators
Go
Aspect ratio
(4)
Verified
Aspect ratio given induced drag factor
Go
Verified
Aspect ratio given span efficiency factor
Go
Verified
Aspect Ratio of Wing given Lift Curve Slope of Elliptic Finite Wing
Go
Verified
Aspect Ratio of Wing given Lift Curve Slope of Finite Wing
Go
1 More Aspect ratio Calculators
Go
Atom
(4)
Created
Angle between incident ray and scattering planes in x-ray diffraction
Go
Verified
Quantization of angular momentum
Go
Created
Spacing between Atomic Lattice Planes in X-ray Diffraction
Go
Created
Wavelength in x-ray diffraction
Go
6 More Atom Calculators
Go
Automobile
(4)
Verified
Mechanical Trail
Go
Verified
Tire Rate given Wheel Rate and Ride Rate
Go
Verified
Total axial force
Go
Verified
Wheel Rate given Tire Rate and Ride Rate
Go
5 More Automobile Calculators
Go
Average power delivered per spark
(3)
Verified
Average energy delivered per spark
Go
Verified
Resistance of charging circuit from average power per spark
Go
Verified
Voltage of power supply from average power per spark
Go
Axial Load
(6)
Created
Axial load of spring for given deflection and stiffness of spring
Go
Created
Axial load on spring given deflection of spring
Go
Created
Axial load on spring given strain energy stored by spring
Go
Created
Axial load on spring given work done on spring
Go
Created
Axial loading on spring
Go
Created
Axial loading on spring given maximum shear stress induced in wire
Go
Axial Load Capacity of Single Piles
(3)
Verified
Allowable load for given safety factor
Go
Verified
Shaft Resistance using Allowable Load and Safety Factor
Go
Verified
Toe Resistance using Allowable Load and Safety Factor
Go
2 More Axial Load Capacity of Single Piles Calculators
Go
Balancing of Rotating Masses
(2)
Created
Angle made by resultant force with horizontal
Go
Created
Resultant centrifugal force
Go
Base Area of Right Circular Cone
(1)
Created
Base Area of Right Circular Cone given Lateral Surface Area and Slant Height
Go
2 More Base Area of Right Circular Cone Calculators
Go
Base Circumference of Right Circular Cone
(2)
Created
Base Circumference of Right Circular Cone given Lateral Surface Area and Slant Height
Go
Created
Base Circumference of Right Circular Cone given Volume and Height
Go
2 More Base Circumference of Right Circular Cone Calculators
Go
BASIC ELECTRICAL MEASUREMENTS
(2)
Verified
Average Transit Angle
Go
Verified
DC Transit Angle
Go
11 More BASIC ELECTRICAL MEASUREMENTS Calculators
Go
Basic electronic Configurations
(8)
Verified
Input resistance
Go
Verified
Input resistance of amplifier
Go
Verified
Input Voltage given Signal voltage
Go
Verified
Output Voltage Gain given Transconductance
Go
Verified
Overall voltage gain
Go
Verified
Overall Voltage Gain given Resistance
Go
Verified
Overall Voltage Gain given Signal Source
Go
Verified
Overall Voltage Gain given Transconductance
Go
6 More Basic electronic Configurations Calculators
Go
Basic Formula
(12)
Verified
Clearance factor in compressor
Go
Verified
Clearance Volume given Clearance Factor
Go
Verified
Compression Ratio given Pressure
Go
Verified
Compression Ratio given Volume
Go
Verified
Discharge Pressure given Compression Ratio
Go
Verified
Discharge Volume given Compression Ratio
Go
Verified
Piston Displacement Volume given Clearance Factor
Go
Verified
Piston Displacement Volume given Volumetric Efficiency in Compressor
Go
Verified
Suction Pressure given Compression Ratio
Go
Verified
Suction Volume given Compression Ratio
Go
Verified
Suction Volume given Volumetric Efficiency in Compressor
Go
Verified
Volumetric efficiency in compressor
Go
Basic Formulas
(3)
Verified
Circumferential stress developed in pipe wall
Go
Verified
Force required to accelerate water in pipe
Go
Verified
Longitudinal Stress developed in Pipe wall
Go
9 More Basic Formulas Calculators
Go
Basic Gain Cell in IC Amplifier
(6)
Verified
Input resistance of active loaded CE amplifier
Go
Verified
Output voltage gain of active loaded CE amplifier
Go
Verified
Output voltage gain of active loaded CS Amplifier
Go
Verified
Output voltage gain of IC Amplifier
Go
Verified
Output voltage gain of IC Amplifier given drain current
Go
Verified
Output voltage gain of IC Amplifier given length of channel
Go
5 More Basic Gain Cell in IC Amplifier Calculators
Go
Basic Gear Parameters
(1)
Verified
Diameter of holes in Gear web of medium size diameter
Go
12 More Basic Gear Parameters Calculators
Go
Basics
(2)
Created
Frequency of oscillation for SHM
Go
Created
Periodic time for SHM
Go
2 More Basics Calculators
Go
Basics
(13)
Created
Angle between axis of radius of rotation and line joining point on curve to origin
Go
Created
Angle between axis of radius of rotation and line joining point on curve to origin O
Go
Created
Corresponding radial force required at each ball for spring loaded governors
Go
Created
Governor power
Go
Created
Height of watt governor
Go
Created
Increased speed
Go
Created
Mean equilibrium angular speed
Go
Created
Mean equilibrium speed in rpm
Go
Created
Ratio of Length of Arm to Length of Link
Go
Created
Sleeve load for decrease in speed value when taking friction into account
Go
Created
Sleeve load for increase in speed value when taking friction into account
Go
Created
Speed of rotation in rpm
Go
Created
Total Downward Force on Sleeve in Wilson-Hartnell Governor
Go
Basics of Amplifier
(1)
Verified
Input to basic amplifier
Go
11 More Basics of Amplifier Calculators
Go
Basics of Centrifugal Pumps
(1)
Verified
Static head
Go
14 More Basics of Centrifugal Pumps Calculators
Go
Basics of Ducts
(6)
Verified
Equivalent Diameter of Circular Duct for Rectangular Duct when Quantity of Air is same
Go
Verified
Equivalent Diameter of Circular Duct for Rectangular Duct when Velocity of Air is same
Go
Verified
Quantity of Air given Velocity
Go
Verified
Reynolds Number given Friction Factor for Laminar Flow
Go
Verified
Reynolds Number in duct
Go
Verified
Velocity Pressure in Ducts
Go
Basics of Gas Turbines
(1)
Verified
Diffuser Efficiency when inlet and exit velocities are present
Go
16 More Basics of Gas Turbines Calculators
Go
Basics Of Physics
(2)
Verified
Average Speed
Go
Verified
Ride rate of car
Go
20 More Basics Of Physics Calculators
Go
Bearing Reactions
(7)
Verified
Force on Crank Pin due to gas pressure inside cylinder
Go
Verified
Horizontal Reaction on Bearing 3 of centre crankshaft at TDC position due to belt tension
Go
Verified
Vertical Reaction on Bearing 1 of centre crankshaft at TDC position due to force on crank pin
Go
Verified
Vertical Reaction on Bearing 1 of centre crankshaft at TDC position given crankweb dimension
Go
Verified
Vertical Reaction on Bearing 2 of centre crankshaft at TDC position due to force on crank pin
Go
Verified
Vertical Reaction on Bearing 2 of centre crankshaft at TDC position due to weight of flywheel
Go
Verified
Vertical Reaction on Bearing 3 of centre crankshaft at TDC position due to weight of flywheel
Go
5 More Bearing Reactions Calculators
Go
Bearing Reactions
(9)
Verified
Horizontal Reaction on Bearing 1 of side crankshaft at TDC position by belt tension given moment
Go
Verified
Horizontal Reaction on Bearing 1 of side crankshaft at TDC position due to belt tension
Go
Verified
Horizontal Reaction on Bearing 2 of side crankshaft at TDC position due to belt tension
Go
Verified
Resultant reaction at Bearing 1 of side crankshaft at TDC position
Go
Verified
Resultant reaction at Bearing 1 of side crankshaft at TDC position given bearing pressure
Go
Verified
Vertical Reaction on Bearing 1 of side crankshaft at TDC position due to force on crank pin
Go
Verified
Vertical Reaction on Bearing 1 of side crankshaft at TDC position due to weight of flywheel
Go
Verified
Vertical Reaction on Bearing 2 of side crankshaft at TDC position due to force on crank pin
Go
Verified
Vertical Reaction on Bearing 2 of side crankshaft at TDC position due to weight of flywheel
Go
1 More Bearing Reactions Calculators
Go
Bearing Reactions
(1)
Verified
Vertical Reaction on Bearing 1 of side crankshaft due to radial force at max torque
Go
7 More Bearing Reactions Calculators
Go
Bearings Reactions
(17)
Verified
Distance between crank pin and centre crankshaft designed at max torque
Go
Verified
Force acting on piston top due to gas pressure for maximum torque on center crankshaft
Go
Verified
Gap of Bearing 2 from Flywheel of centre crankshaft at max torque position
Go
Verified
Gap of Bearing 3 from Flywheel of centre crankshaft at max torque position
Go
Verified
Horizontal Reaction on Bearing 1 of centre crankshaft due to tangential force at max torque
Go
Verified
Horizontal Reaction on Bearing 2 of centre crankshaft due to belt tension at max torque
Go
Verified
Horizontal Reaction on Bearing 2 of centre crankshaft due to tangential force at max torque
Go
Verified
Horizontal Reaction on Bearing 3 of centre crankshaft due to belt tension at max torque
Go
Verified
Resultant Reaction on Bearing 1 of centre crankshaft at angle of max torque
Go
Verified
Resultant Reaction on Bearing 2 of centre crankshaft at angle of max torque
Go
Verified
Resultant Reaction on Bearing 3 of centre crankshaft at angle of max torque
Go
Verified
Tangential component of force at crank pin given horizontal reaction on bearing 1
Go
Verified
Tangential component of force at crank pin given horizontal reaction on bearing 2
Go
Verified
Vertical Reaction on Bearing 1 of centre crankshaft due to radial force at max torque
Go
Verified
Vertical Reaction on Bearing 2 of centre crankshaft due to flywheel weight at max torque
Go
Verified
Vertical Reaction on Bearing 2 of centre crankshaft due to radial force at max torque
Go
Verified
Vertical Reaction on Bearing 3 of centre crankshaft due to flywheel weight at max torque
Go
1 More Bearings Reactions Calculators
Go
Belt Drive
(20)
Created
Angle made by belt with vertical axis for cross belt drive
Go
Created
Angle made by belt with vertical axis for open belt drive
Go
Created
Angle of contact for cross belt drive
Go
Created
Angle of contact for open belt drive
Go
Created
Centrifugal Tension in Belt
Go
Created
Cross belt drive length
Go
Created
Frictional force in V belt drive
Go
Created
Initial Tension in Belt
Go
Verified
Length of Belt that passes over Driver
Go
Verified
Length of Belt that passes over Follower
Go
Created
Length of Open Belt Drive
Go
Created
Maximum tension for transmission of maximum power by belt
Go
Created
Maximum tension of belt
Go
Created
Normal Reaction between Belt and Sides of Groove
Go
Created
Power transmitted by belt
Go
Created
Relation between pitch and pitch circle diameter of chain drive
Go
Created
Torque Exerted on Driven Pulley
Go
Created
Torque Exerted on Driving Pulley
Go
Created
Total percentage slip in belt
Go
Created
Velocity for transmission of maximum power by belt
Go
Bending Moment
(6)
Created
Bending moment at center given point load acting at center of spring load
Go
Created
Bending moment at center of leaf spring
Go
Created
Bending moment on each plate given total resisting moment by n plates
Go
Created
Bending moment on single plate
Go
Created
Maximum bending moment developed in plate given bending moment on single plate
Go
Created
Maximum bending moment developed in plate given total resisting moment by n plates
Go
Bending Stress in Lever
(5)
Verified
Bending stress in lever of elliptical cross section
Go
Verified
Bending stress in lever of elliptical cross section given bending moment
Go
Verified
Bending stress in lever of rectangular cross section
Go
Verified
Bending stress in lever of rectangular cross section given bending moment
Go
Verified
Maximum bending moment in lever
Go
Bernie's and Clavarino's Equation
(4)
Verified
Inner Diameter of Pressurized Cylinder from Bernie's Equation
Go
Verified
Inner Diameter of Pressurized Cylinder from Clavarino's Equation
Go
Verified
Thickness of Pressurized Cylinder from Bernie's Equation
Go
Verified
Thickness of Pressurized Cylinder from Clavarino's Equation
Go
Biaxial Stress Deformation System
(2)
Created
Strain in x direction in biaxial system
Go
Created
Strain in Y direction in biaxial system
Go
Big and Small End Bearings
(9)
Verified
Bearing pressure on crank pin bush
Go
Verified
Bearing pressure on piston pin bush
Go
Verified
Crank radius given stroke length of piston
Go
Verified
Mass of reciprocating parts in engine cylinder
Go
Verified
Maximum force acting on crank pin bearing given allowable bearing pressure
Go
Verified
Maximum force acting on piston pin bearing
Go
Verified
Maximum force acting on piston pin bearing given allowable bearing pressure
Go
Verified
Maximum height of connecting rod at big end
Go
Verified
Minimum height of connecting rod at big end
Go
3 More Big and Small End Bearings Calculators
Go
Big End Cap and Bolts
(11)
Verified
Bending moment on big end cap of connecting rod
Go
Verified
Core diameter of bolts of big end cap of connecting rod
Go
Verified
Inertia Force on Bolts of Connecting Rod
Go
Verified
Mass of connecting rod
Go
Verified
Maximum bending moment on connecting rod
Go
Verified
Maximum bending stress in big end cap of connecting rod
Go
Verified
Maximum Inertia force on bolts of connecting rod
Go
Verified
Maximum Inertia force on bolts of connecting rod given permissible tensile stress of bolts
Go
Verified
Span length of big end cap of connecting rod
Go
Verified
Thickness of big end cap of connecting rod given bending stress in cap
Go
Verified
Width of big end cap of connecting rod given bending stress in cap
Go
BJT
(10)
Verified
3 dB frequency of STC circuit
Go
Verified
Depletion capacitance of BJT
Go
Verified
Finite input voltage of BJT at unity gain frequency
Go
Verified
Finite input voltage of BJT at unity gain frequency given complex frequency variable
Go
Verified
Short circuit current gain of BJT
Go
Verified
Signal Current in Collector
Go
Verified
Transition frequency of BJT
Go
Verified
Transition frequency of BJT given device constant
Go
Verified
Unity-gain bandwidth
Go
Verified
Unity-gain bandwidth of BJT
Go
6 More BJT Calculators
Go
BJT Case
(3)
Verified
Common mode gain of BJT
Go
Verified
Common mode input resistance of BJT half-circuit
Go
Verified
Common mode rejection ratio of BJT
Go
BJT Differential Pair
(11)
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 transconductance
Go
Verified
First base emitter voltage of BJT differential amplifier
Go
Verified
First emitter current of BJT differential amplifier
Go
Verified
Maximum input common-mode range voltage of BJT differential amplifier
Go
Verified
Second base-emitter voltage of BJT differential amplifier
Go
Verified
Second collector current of BJT differential amplifier
Go
Verified
Signal current of BJT differential amplifier
Go
Verified
Transconductance of small signal operation of BJT Amplifier given total current
Go
5 More BJT Differential Pair Calculators
Go
Blood Differential Test
(1)
Verified
Absolute Neutrophil Count
Go
4 More Blood Differential Test Calculators
Go
Bolt Loads in Gasket Joints
(16)
Verified
Actual Cross-sectional Area of Bolts given Root Diameter of Thread
Go
Verified
Bolt Load in Design of Flange for Gasket Seating
Go
Verified
Bolt load under operating condition
Go
Verified
Bolt Load under operating condition given Hydrostatic End Force
Go
Verified
Deflection of Spring Initial Bolt Load to Seal Gasket Joint
Go
Verified
Gasket Width given actual Cross-sectional Area of Bolts
Go
Verified
Hydrostatic Contact Force given Bolt Load under Operating condition
Go
Verified
Hydrostatic end force
Go
Verified
Hydrostatic End Force given Bolt Load under Operating condition
Go
Verified
Initial Bolt Load to seat Gasket Joint
Go
Verified
Load on bolts based on hydrostatic end force
Go
Verified
Stress Required for Gasket Seating
Go
Verified
Stress Required for Gasket Seating given Bolt Load
Go
Verified
Test pressure given Bolt Load
Go
Verified
Total cross-sectional area of bolt at root of thread
Go
Verified
Width of U Collar given Initial Bolt Load to Seat Gasket Joint
Go
Bolted Joints
(10)
Verified
Core Diameter of Bolt given Shear Area of Nut
Go
Verified
Core Diameter of Bolt given Tensile Force on Bolt in Shear
Go
Verified
Height of Nut given Shear Area of Nut
Go
Verified
Height of Nut given Strength of Bolt in Shear
Go
Verified
Height of Standard Nut
Go
Verified
Nominal Diameter of Bolt given Height of Standard Nut
Go
Verified
Shear Area of Nut
Go
Verified
Tensile Force on Bolt in Shear
Go
Verified
Yield Strength of Bolt in Shear given Tensile Force on Bolt in Shear
Go
Verified
Yield Strength of Bolt in Tension given Tensile Force on Bolt in Shear
Go
9 More Bolted Joints Calculators
Go
Bolts and stresses in flange joints
(10)
Verified
Bolt Load given Flange pressure
Go
Verified
Bolt Load given Modulus of Elasticity and Increment Length
Go
Verified
Bolt load in gasket joint
Go
Verified
Flange pressure developed due to tightening of bolt
Go
Verified
Flange pressure given Twisting moment
Go
Verified
Gasket Area given Flange pressure
Go
Verified
Initial Bolt Torque given Bolt Load
Go
Verified
Nominal Bolt Diameter given Bolt Load
Go
Verified
Number of Bolts given Flange pressure
Go
Verified
Twisting Moment given Flange Pressure
Go
Bore and Length of Engine Cylinder
(7)
Verified
Bore of engine cylinder given length
Go
Verified
Gas Force acting on cylinder cover
Go
Verified
Indicated mean effective pressure
Go
Verified
Length of engine cylinder given cylinder bore
Go
Verified
Length of engine cylinder given stroke length
Go
Verified
Maximum gas pressure inside engine cylinder
Go
Verified
Stroke length of engine given length of cylinder
Go
Bottom Weld
(24)
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
Brake
(5)
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
Brake Power
(6)
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
Braking Torque
(12)
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
Buckling of Connecting Rod
(11)
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
Butt Joints
(1)
Verified
Transverse Shrinkage in Butt Joints
Go
13 More Butt Joints Calculators
Go
By-pass Factor of Heating and Cooling coil
(7)
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
Cam and Follower
(19)
Created
Condition for contact of roller if straight flank merges into nose(tangent cam with roller follower)
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
Displacement of needle for tangent cam with needle-bearing follower
Go
Created
Displacement of roller of tangent cam with roller follower, when there's nose contact
Go
Created
Distance between roller center and nose center of tangent cam with roller follower
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 on diameter for SHM of follower
Go
Created
Peripheral speed of projection of point P'(which is projection of point P on dia)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
Created
Velocity of follower for roller follower tangent cam if contact is with straight flanks
Go
Created
Velocity of follower of roller follower tangent cam for contact with nose
Go
Capacitor
(6)
Verified
Capacitance of cylindrical capacitor
Go
Verified
Capacitance of parallel plate capacitor
Go
Verified
Capacitance of spherical capacitor
Go
Verified
Current density given conductivity
Go
Verified
Equivalent capacitance for two capacitors in parallel
Go
Verified
Equivalent capacitance for two capacitors in series
Go
13 More Capacitor Calculators
Go
Casting Yield
(1)
Verified
Casting yield
Go
3 More Casting Yield Calculators
Go
CC-CB and CD-CG Configurations
(7)
Verified
3 dB frequency of CC CB amplifier
Go
Verified
First pole frequency of CC CB amplifier
Go
Verified
Input resistance of CC CB amplifier
Go
Verified
Input resistance when emitter resistances are equal in CC-CB amplifier
Go
Verified
Overall voltage gain of CC CB amplifier
Go
Verified
Second pole frequency of CC-CB amplifier
Go
Verified
Voltage gain of CC-CB amplifier
Go
Centrifugal Force
(9)
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
Change in Dimension of Thin Spherical Shell due to Internal Pressure
(17)
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
Change in Dimensions
(12)
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
Charging time
(5)
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
Charging voltage
(2)
Verified
Charging voltage for maximum power of spark
Go
Verified
Power supply for maximum power of spark
Go
6 More Charging voltage Calculators
Go
Chip Break distance
(2)
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
Chip control
(2)
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
Circular Curves
(21)
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 Calculators
Go
Circular Section
(6)
Created
Diameter of circular section for given moment of inertia about neutral axis
Go
Created
Diameter of circular section for given section modulus
Go
Created
Diameter of Circular Section given Distance of Outermost Layer from Neutral Layer
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
Circular Section
(19)
Created
Average shear force for circular section
Go
Created
Average shear stress for circular section
Go
Created
Average Shear Stress for Circular Section using Maximum Shear Stress
Go
Created
Maximum Shear Force using Radius of Circular Section
Go
Created
Maximum shear stress for circular section
Go
Created
Maximum Shear Stress for Circular Section using Average Shear Stress
Go
Created
Maximum Shear Stress using Radius of Circular Section
Go
Created
Moment of inertia of circular section
Go
Created
Moment of Inertia of Circular Section given Shear Stress
Go
Created
Moment of Inertia of Circular Section using Maximum Shear Stress
Go
Created
Moment of Shaded Area (area above considered layer) about Neutral Axis
Go
Created
Radius of Circular Section given Width of Beam at Considered Level
Go
Created
Radius of Circular Section using Average Shear Stress
Go
Created
Radius of Circular Section using Maximum Shear Stress
Go
Created
Shear force distribution for circular section
Go
Created
Shear Force using Maximum Shear Stress
Go
Created
Shear stress distribution for circular section
Go
Created
Width of Beam at Considered Level using Radius of Circular Section
Go
Created
Width of Beam at Considered Level using Shear Stress for Circular Section
Go
Circulation
(1)
Verified
Circulation for rotating cylinders
Go
3 More Circulation Calculators
Go
Circulation at the origin
(4)
Verified
Circulation at Origin given Downwash
Go
Verified
Circulation at Origin given Induced Angle of Attack
Go
Verified
Circulation at Origin given Lift of Wing
Go
Verified
Circulation at Origin in Elliptical Lift Distribution
Go
Circumferential Stress And Strain
(7)
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
Circumscribed Cone
(7)
Created
Base length of parabolic section that can be cut from cone for maximum area of parabolic section
Go
Created
Distance from minor arc of Cone of parabolic section cut from cone for maximum area
Go
Created
Height of Cone circumscribing sphere such that volume of cone is minimum
Go
Created
Height of parabolic section that can be cut from cone for maximum area of parabolic section
Go
Created
Maximum area of parabolic segment that can be cut from Cone
Go
Created
Radius of Cone circumscribing sphere such that volume of cone is minimum
Go
Created
Volume of Cone circumscribing sphere such that volume of cone is minimum
Go
Circumscribed Cylinder
(2)
Created
Surface area of Cylinder circumscribing sphere given radius of sphere
Go
Created
Volume of Cylinder circumscribing sphere given radius of sphere
Go
2 More Circumscribed Cylinder Calculators
Go
Circumscribed Sphere
(4)
Created
Diameter of Circumscribing Sphere given diameter and height of circumscribed cylinder
Go
Created
Radius of Sphere circumscribing cube given cube side
Go
Created
Surface area of Sphere circumscribing cylinder
Go
Created
Volume of Sphere circumscribing cube given cube side
Go
1 More Circumscribed Sphere Calculators
Go
Class A Output Stage
(22)
Verified
Average load power of class A output stage
Go
Verified
Average load power of output stage
Go
Verified
Average supply power of output stage
Go
Verified
Bias current in minimum transfer characteristics of emitter-follower in negative limit
Go
Verified
Bias current of emitter follower
Go
Verified
Collector current at instantaneous power dissipation in transistor
Go
Verified
Condition of maximum efficiency of emitter follower
Go
Verified
Condition of maximum power conversion efficiency
Go
Verified
Instantaneous power dissipation of emitter-follower
Go
Verified
Load power of output stage
Go
Verified
Maximum transfer characteristics of emitter-follower in positive limit
Go
Verified
Maximum voltage of emitter-follower when transistor saturates
Go
Verified
Minimum transfer characteristics of emitter-follower in negative limit
Go
Verified
Minimum voltage of emitter-follower when transistor saturates
Go
Verified
Peak output voltage value at average load power
Go
Verified
Power conversion efficiency of class A output stage
Go
Verified
Power conversion efficiency of output-stage
Go
Verified
Saturation voltage between collector-emitter at maximum voltage
Go
Verified
Saturation voltage between collector-emitter at minimum voltage
Go
Verified
Supply power of output stage
Go
Verified
Transfer characteristics of emitter-follower
Go
Verified
Voltage between collector-emitter at instantaneous power dissipation
Go
Class B Output Stage
(18)
Verified
Average load-power of class B stage
Go
Verified
Average power dissipation in class B stage
Go
Verified
Average power dissipation in class B stage given supply power
Go
Verified
Efficiency of class B output stage
Go
Verified
Efficiency of class B stage
Go
Verified
Load power in class B stage given average power dissipation
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
Output sinusoid peak voltage of class B stage
Go
Verified
Peak voltage at maximum power dissipation
Go
Verified
Positive half of maximum power dissipation in class B stage
Go
Verified
Power drain from positive sine wave
Go
Verified
Power drawn from negative sine wave
Go
Verified
Supply power in class B stage given average power dissipation
Go
Verified
Supply voltage at maximum power dissipation
Go
Verified
Total power supply of class B stage
Go
Coil Spring
(5)
Verified
Compressed length of coil spring
Go
Verified
Pitch of coil spring
Go
Verified
Total axial gap between coils of spring
Go
Verified
Wire diameter of inner spring given wire diameter of outer spring and spring index
Go
Verified
Wire diameter of outer spring given wire diameter of inner spring and spring index
Go
3 More Coil Spring Calculators
Go
Cold Formed or Light Weighted Steel Structures
(2)
Verified
Allowable Design Strength
Go
Verified
Nominal Strength using Allowable Design Strength
Go
13 More Cold Formed or Light Weighted Steel Structures Calculators
Go
Columns With Eccentric Load
(22)
Created
Cross sectional area of column given maximum stress for column with eccentric load
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
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
Columns With Initial Curvature
(19)
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
Combinational Circuit Design
(1)
Verified
X Voltage NAND Gate
Go
Common Mode Rejection Ratio(CMRR)
(5)
Verified
Collector current of BJT differential amplifier given emitter resistance
Go
Verified
First collector current of BJT differential amplifier
Go
Verified
Minimum input common-mode range of BJT differential amplifier
Go
Verified
Second emitter resistance of BJT differential amplifier
Go
Verified
Transconductance of small signal operation of BJT Amplifier
Go
6 More Common Mode Rejection Ratio(CMRR) Calculators
Go
Common-Emitter Amplifier
(4)
Verified
High frequency gain of CE amplifier given signal resistance
Go
Verified
Mid band gain of CE Amplifier
Go
Verified
Signal resistance in high frequency response of CE amplifier
Go
Verified
Signal Resistance of CE amplifier
Go
6 More Common-Emitter Amplifier Calculators
Go
Common-Gate and Common-Base Amplifiers
(1)
Verified
Output Voltage given Transconductance
Go
14 More Common-Gate and Common-Base Amplifiers Calculators
Go
Common-Source Amplifier
(2)
Verified
Input resistance of common source amplifier
Go
Verified
Output resistance of common source amplifier
Go
1 More Common-Source Amplifier Calculators
Go
Common-Source Amplifier
(17)
Verified
Break frequency of single time constant circuit
Go
Verified
Corner frequency of single time constant circuit
Go
Verified
Current supplied through small capacitance in CS Amplifier
Go
Verified
Equivalent capacitance between gate and ground of CS amplifier
Go
Verified
Equivalent resistance of CS amplifier
Go
Verified
Equivalent signal resistance of CS amplifier
Go
Verified
High frequency gain of CS Amplifier
Go
Verified
High frequency response of CS Amplifier
Go
Verified
High-frequency response given input capacitance
Go
Verified
Input capacitance of single time constant circuit
Go
Verified
Mid band gain of CS Amplifier given resistance
Go
Verified
Midband gain of CS Amplifier
Go
Verified
Output voltage of CS amplifier
Go
Verified
Output voltage of single time constant circuit
Go
Verified
Resistance across capacitor of bipolar cascode amplifier
Go
Verified
Signal resistance of bipolar cascode amplifier
Go
Verified
Upper 3-dB frequency
Go
2 More Common-Source Amplifier Calculators
Go
Compound Cylinder Shrinkage Radii Change
(21)
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
Compound Pendulum
(3)
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
Concentrating Collectors
(5)
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
Concentric Springs
(1)
Verified
Axial Force transmitted by Inner Spring
Go
10 More Concentric Springs Calculators
Go
Conceptual Design
(13)
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
Condensers
(1)
Verified
Heat Rejection Factor
Go
4 More Condensers Calculators
Go
Conduction Shape Factors for different Configurations
(13)
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
Isothermal Ellipsoid buried in Infinite Medium
Go
Verified
Isothermal rectangular parallelepiped buried in semi-infinite medium
Go
Verified
Isothermal Sphere buried in Infinite Medium
Go
Verified
Isothermal sphere buried in semi-infinite medium
Go
Verified
Long hollow cylindrical layer
Go
Verified
Row of Equally spaced Parallel Isothermal Cylinders buried in Semi-infinite medium
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
Verified
Thin rectangular plate buried in semi-infinite medium
Go
Verified
Vertical isothermal cylinder buried in semi-infinite medium
Go
8 More Conduction Shape Factors for different Configurations Calculators
Go
Constants
(25)
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
Continuity Equation for Ducts
(4)
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
Continuity equation for normal shock waves
(4)
Verified
Density downstream of shock wave using continuity equation
Go
Verified
Density upstream of shock wave using continuity equation
Go
Verified
Flow velocity downstream of shock wave using continuity equation
Go
Verified
Flow velocity upstream of shock wave using continuity equation
Go
Contribution of Aircraft Components- Part 1
(9)
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
Contribution of Aircraft Components- Part 2
(9)
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
Contribution of Aircraft Components- Part 3
(7)
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
Contribution of Aircraft Components- Part 4
(2)
Verified
Sideslip angle for yawing moment coefficient given vertical tail volume ratio
Go
Verified
Sidewash angle for given yawing moment coefficient
Go
Controlling Force
(5)
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
Convection Coefficient
(7)
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
Convective Mass Transfer
(10)
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
Cooling Loads
(1)
Verified
Cooling load from lighting
Go
10 More Cooling Loads Calculators
Go
Core Diameter
(1)
Verified
Core diameter of Bolt given Tensile Stress
Go
3 More Core Diameter Calculators
Go
Cores - Core Prints and Chaplets
(2)
Verified
Buoyant force on cores
Go
Verified
Volume of core
Go
11 More Cores - Core Prints and Chaplets Calculators
Go
Cornering
(7)
Verified
Corner Radius given Effective Weight of Car due to Banking
Go
Verified
Corner radius given horizontal lateral acceleration
Go
Verified
Cornering Velocity given Effective Weight of Car due to Banking
Go
Verified
Cornering velocity given horizontal lateral acceleration
Go
Verified
Effective Weight of Car due to Banking
Go
Verified
Horizontal Lateral Acceleration
Go
Verified
Total static mass of car given effective weight during banking
Go
5 More Cornering Calculators
Go
Criterion for arcing
(4)
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
Critical or Whirling Speed of a Shaft
(12)
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
Cross-Sectional Area of Socket and Spigot
(3)
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
Cryogenic Systems
(1)
Created
Debye Temperature
Go
Cube
(8)
Created
Curved Surface Area of Largest right circular cylinder within cube for given side of cube
Go
Created
Lateral Surface Area of Cube given Face Diagonal
Go
Created
Radius of Largest Right Circular Cylinder within Cube given Side of Cube
Go
Created
Radius of Sphere inscribing Cube given Cube side
Go
Created
Total Surface Area of Cube given Face Area
Go
Created
Total Surface Area of largest right circular cylinder within cube
Go
Created
Volume of Cube
Go
Created
Volume of Largest Right Circular Cylinder within Cube given Side of Cube
Go
Cuboid
(2)
Created
Lateral Surface Area of Cuboid
Go
Created
Total Surface Area of Cuboid
Go
Current & Voltage
(4)
Verified
Input bias current of differential amplifier
Go
Verified
Input bias current of differential amplifier given common emitter current gain
Go
Verified
Input offset current of differential amplifier
Go
Verified
Input offset current of differential amplifier given common emitter current gain
Go
Current and Voltage Characteristics of Transistor
(1)
Verified
Total power supplied in BJT
Go
4 More Current and Voltage Characteristics of Transistor Calculators
Go
Current Electricity
(6)
Verified
Current density given electric current and area
Go
Verified
Current Density given resistivity
Go
Verified
Electric Current given charge and time
Go
Verified
Electric Current given Drift Velocity
Go
Verified
Power given electric current and resistance
Go
Verified
Power given electric potential difference and resistance
Go
15 More Current Electricity Calculators
Go
Current-Mirror Circuits with Improved Performance
(5)
Verified
Emitter resistance of Widlar Current Source
Go
Verified
Output current of Wilson current mirror
Go
Verified
Output resistance of Cascode MOS Mirrors
Go
Verified
Output resistance of Widlar Current Source
Go
Verified
Output resistance of Wilson current mirror
Go
3 More Current-Mirror Circuits with Improved Performance Calculators
Go
Cutting fluid and Surface Roughness
(4)
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
Cutting Force
(2)
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
Cylinder Head and its Studs
(12)
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
Cylindrical Grinding cycle
(1)
Verified
Width of Grinding path given number of workpiece revolutions
Go
16 More Cylindrical Grinding cycle Calculators
Go
DC Offset
(4)
Verified
Input Offset Voltage of MOS Differential Amplifier
Go
Verified
Input Offset Voltage of MOS Differential Amplifier given transconductance
Go
Verified
Input Offset Voltage of MOS Differential Amplifier when aspect ratio mismatches
Go
Verified
Total Input Offset Voltage of MOS Differential Amplifier
Go
3 More DC Offset Calculators
Go
Dedendum Circle Diameter
(1)
Verified
Dedendum Circle Diameter of Large Size Gear
Go
4 More Dedendum Circle Diameter Calculators
Go
Deflection
(7)
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 end 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
Degree of Saturation
(5)
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 vapour in saturated air given degree of saturation
Go
Verified
Total pressure of moist air given degree of saturation
Go
Density Of Disc
(9)
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
Depth of Groove
(4)
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
Design Of A Riveted Joint
(14)
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
Design of Bearings
(11)
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
Design of Bevel Gear
(14)
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
Design of Bushed-Pin flexible coupling
(2)
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
Design of clamp coupling
(2)
Verified
Tensile force on each bolt of Clamp Coupling
Go
Verified
Tensile force on each bolt of Clamp Coupling given Torque
Go
4 More Design of clamp coupling Calculators
Go
Design of Crank Pin
(9)
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
Design of Crank Pin
(6)
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
Design of Crank Pin
(9)
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
Design of Crank Pin
(4)
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
Design of Crank Web
(14)
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
Design of Crank Web
(8)
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
Design of Crank Web
(9)
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
Design of Crank Web
(9)
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
Design of Crankshaft Bearing
(3)
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
Design of Cross Section of Rocker Arm
(4)
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
Design of Curved Beams
(18)
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
Design of Flywheel
(5)
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
Design of Forked End
(12)
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
Design of Fulcrum Pin
(8)
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
Design of Fulcrum Pin
(8)
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
Design of Hollow Shaft
(4)
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
Design of Machine Elements
(2)
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
Design of Muff coupling
(2)
Verified
Diameter of Driving Shaft of Muff Coupling given Outer diameter of sleeve
Go
Verified
Outer diameter of sleeve of Muff Coupling
Go
2 More Design of Muff coupling Calculators
Go
Design of Pressure Vessels
(6)
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
Design of Rolling Contact Bearing
(12)
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
Design of Shaft for Torsional Moment
(4)
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
Design of Shaft Under Flywheel
(8)
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
Design of Shaft Under Flywheel
(1)
Verified
Torsional moment at central plane of centre crankshaft below flywheel at max torque
Go
5 More Design of Shaft Under Flywheel Calculators
Go
Design of Shaft Under Flywheel
(6)
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
Design of Tappet
(5)
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
Design of Worm Gear
(1)
Verified
Diametral Quotient of Worm Gear
Go
6 More Design of Worm Gear Calculators
Go
Deviation of Shear Stress produced in a Circular Shaft subjected to Torsion
(17)
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
Diameter of Pin of Knuckle joint
(9)
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
Diameter of Push Rod
(6)
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
Diameter of Rivet
(7)
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
Go
Diameter of Rod of Cotter Joint
(4)
Verified
Diameter of rod of cotter joint given socket collar diameter
Go
Verified
Diameter of rod of cotter joint given spigot collar diameter
Go
Verified
Diameter of rod of cotter joint given thickness of cotter
Go
Verified
Diameter of rod of cotter joint given thickness of spigot collar
Go
1 More Diameter of Rod of Cotter Joint Calculators
Go
Diameter of Rod Of Knuckle Joint
(5)
Verified
Diameter of Rod of knuckle joint given its Enlarged Diameter near joint
Go
Verified
Diameter of Rod of knuckle joint given tensile stress in Rod
Go
Verified
Enlarged Diameter of Rod of knuckle joint near joint
Go
Verified
Rod diameter of knuckle joint given thickness of eye
Go
Verified
Rod diameter of knuckle joint given thickness of fork eye
Go
Diameter of Socket Collar
(4)
Verified
Diameter of socket collar of cotter joint given bending stress in cotter
Go
Verified
Diameter of socket collar of cotter joint given compressive stress
Go
Verified
Diameter of socket collar of cotter joint given shear stress in socket
Go
Verified
Inside diameter of socket of cotter joint given shear stress in socket
Go
1 More Diameter of Socket Collar Calculators
Go
Diameter of Spigot and Spigot Collar
(3)
Verified
Diameter of spigot of cotter joint given bending stress in cotter
Go
Verified
Diameter of spigot of cotter joint given compressive stress
Go
Verified
Diameter of spigot of cotter joint given shear stress in spigot
Go
3 More Diameter of Spigot and Spigot Collar Calculators
Go
Diameter of Spring
(5)
Created
Diameter of spring wire given deflection of spring
Go
Created
Diameter of spring wire given maximum shear stress induced in wire
Go
Created
Diameter of spring wire given stiffness of helical spring
Go
Created
Diameter of spring wire given strain energy stored by spring
Go
Created
Diameter of spring wire given twisting moment
Go
Diameter of Spring Wire
(6)
Verified
Diameter of wire of engine valve spring
Go
Verified
Diameter of wire of engine valve spring given maximum compression in spring
Go
Verified
Diameter of wire of engine valve spring given number of active turns of spring
Go
Verified
Spring Index of engine valve spring given shear stress, maximum force and wire diameter
Go
Verified
Wahl factor for engine valve spring given mean coil diameter and wire diameter
Go
Verified
Wahl factor for engine valve spring given spring index
Go
3 More Diameter of Spring Wire Calculators
Go
Diameter of Wire
(7)
Created
Diameter of wire given bursting force due to fluid pressure
Go
Created
Diameter of wire given compressive circumferential stress exerted by wire
Go
Created
Diameter of wire given initial tensile force and length of wire
Go
Created
Diameter of wire given initial tensile force in wire
Go
Created
Diameter of wire given number of turns of wire in length L
Go
Created
Diameter of wire given resisting force of wire per cm length
Go
Created
Diameter of wire given resisting force on wire
Go
Differential Amplifier with Current-Mirror Load
(14)
Verified
Common-mode gain of controlled source transistor
Go
Verified
Common-mode gain of controlled source transistor given voltage gain
Go
Verified
Current gain of controlled source transistor
Go
Verified
Differential gain of MOS with Current-Mirror Load given transconductance
Go
Verified
Differential gain of MOS with Current-Mirror Load when resistances at different drain are equal
Go
Verified
Differential input resistance of MOS with Current-Mirror Load
Go
Verified
Differential voltage gain when short circuit transconductance equals to transconductance
Go
Verified
Offset voltage of MOSFET of MOS with Current-Mirror Load
Go
Verified
Offset voltage of MOSFET with Current-Mirror Load
Go
Verified
Output resistance at another drain of controlled source transistor
Go
Verified
Output resistance of controlled source transistor
Go
Verified
Output voltage of controlled source transistor
Go
Verified
Short circuit transconductance of MOS transistor with controlled source
Go
Verified
Short circuit transconductance of MOS transistor with controlled source given resistance
Go
9 More Differential Amplifier with Current-Mirror Load Calculators
Go
Dimensionless groups
(6)
Verified
Bingham Number
Go
Verified
Buoyant force given grashof number
Go
Verified
Eckert Number
Go
Verified
Heat diffusivity given Lewis number
Go
Verified
Modified Rayleigh number given Bingham number
Go
Verified
Viscous force given grashofs number
Go
14 More Dimensionless groups Calculators
Go
Dimensionless Numbers
(1)
Verified
Grashof Number
Go
10 More Dimensionless Numbers Calculators
Go
Dimensionless Performance Parameters
(8)
Verified
Coefficient of Friction in Terms of Coefficient of friction Variable
Go
Verified
Coefficient of Friction Variable of Bearing in Terms of Coefficient of Friction
Go
Verified
Flow Ratio Variable in Terms of Outflow of Lubricant
Go
Verified
Flow Variable in Terms of Flow of Lubricant in Clearance Space of Journal
Go
Verified
Load Coefficient in Terms of Load Acting on Bearing
Go
Verified
Radial Clearance in Terms of Coefficient of Friction Variable of Bearing
Go
Verified
Radius of Journal in Terms of Coefficient of Friction Variable
Go
Verified
Sommerfeld Number of Bearing
Go
Dimensions of Lever Arm
(6)
Verified
Angle between arms of lever given effort, load and net reaction at fulcrum
Go
Verified
Depth of lever arm given width
Go
Verified
Length of major axis for elliptical cross sectioned lever given minor axis
Go
Verified
Length of minor axis for elliptical cross sectioned lever given major axis
Go
Verified
Outside diameter of boss in lever
Go
Verified
Width of lever arm given depth
Go
Direct Count System
(2)
Verified
Direct Count
Go
Verified
Tex Count
Go
3 More Direct Count System Calculators
Go
Direct Strains of Diagonal
(11)
Verified
Modulus of Rigidity using Young's Modulus and Poisson's Ratio
Go
Verified
Poisson's ratio given tensile strain due to compressive stress in diagonal BD
Go
Verified
Poisson's Ratio using Modulus of Rigidity
Go
Verified
Shear Strain in Diagonal given Tensile Strain for Square Block
Go
Verified
Tensile strain in diagonal BD of square block ABCD due to compressive stress
Go
Verified
Tensile Strain in Diagonal given Shear Strain for Square Block
Go
Verified
Tensile Strain in Diagonal of Square Block due to Tensile Stress
Go
Verified
Total Compressive Strain in Diagonal AC of Square Block ABCD
Go
Verified
Total tensile strain in diagonal BD of square block ABCD given modulus of rigidity
Go
Verified
Total Tensile Strain in Diagonal of Square Block
Go
Verified
Young's Modulus using Modulus of Rigidity
Go
Discharge
(2)
Verified
Rate of flow of liquid into air vessel
Go
Verified
Rate of Flow of Liquid into Air Vessel given Stroke Length
Go
3 More Discharge Calculators
Go
Discharging current
(3)
Verified
Discharge current
Go
Verified
Discharge voltage
Go
Verified
Resistance of discharging circuit discharge voltage
Go
Discharging voltage
(5)
Verified
Capacitance of circuit from resistance of discharging circuit
Go
Verified
Discharging voltage
Go
Verified
Resistance of discharging circuit from capacitance
Go
Verified
Time elapsed
Go
Verified
Voltage of charging circuit
Go
Distance
(4)
Verified
Distance from start given restoring force and constant k
Go
Verified
Distance traveled by particle in shm when velocity becomes zero
Go
Verified
Distance traveled given velocity
Go
Verified
Distance traveled in SHM given angular frequency
Go
Distortion Energy Theory
(6)
Verified
Shear yield strength by maximum distortion energy theorem
Go
Verified
Strain energy corresponding to distortion with no change in volume
Go
Verified
Strain energy corresponding to distortion with no change in volume given yield strength
Go
Verified
Tensile yield strength by distortion energy theorem considering factor of safety for biaxial stress
Go
Verified
Tensile yield strength from distortion energy theorem
Go
Verified
Tensile yield strength from distortion energy theorem considering factor of safety
Go
7 More Distortion Energy Theory Calculators
Go
Draft Tube
(4)
Verified
Efficiency of draft tube
Go
Verified
Head loss in draft tube given efficiency
Go
Verified
Velocity of water at inlet of draft tube given draft tube efficiency
Go
Verified
Velocity of water at outlet of draft tube given draft tube efficiency
Go
Drag Coefficients for finite wings
(5)
Verified
Induced drag coefficient
Go
Verified
Induced drag coefficient given total drag coefficient
Go
Verified
Profile drag coefficient
Go
Verified
Profile drag coefficient given total drag coefficient
Go
Verified
Total drag coefficient for subsonic finite wing
Go
Drag Force on Body
(3)
Verified
Buoyant force acting on spherical ball
Go
Verified
Drag Force for body moving in Fluid
Go
Verified
Power Required to Keep Flat Plate in Motion
Go
4 More Drag Force on Body Calculators
Go
Driveline
(5)
Verified
Axial force of multiplate clutch using uniform wear theory
Go
Verified
Effective gear ratio
Go
Verified
Final drive ratio
Go
Verified
Torque transmitted by n friction surfaces
Go
Verified
Torque transmitted by n friction surfaces using uniform wear theory
Go
13 More Driveline Calculators
Go
Dynamic Load
(6)
Verified
Dynamic Load Capacity for Ball Bearing
Go
Verified
Dynamic Load Capacity for Bearing given Rated Bearing Life
Go
Verified
Dynamic Load Capacity for Roller Bearing
Go
Verified
Equivalent Dynamic Load for Ball Bearing
Go
Verified
Equivalent Dynamic Load for Bearing given Rated Bearing Life
Go
Verified
Equivalent Dynamic Load for Roller Bearing
Go
1 More Dynamic Load Calculators
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Dynamic loss in ducts
(12)
Verified
Dynamic Loss Coefficient given Dynamic Pressure Loss
Go
Verified
Dynamic Loss Coefficient given Equivalent Additional Length
Go
Verified
Dynamic Pressure loss
Go
Verified
Pressure Loss at Discharge or Exit
Go
Verified
Pressure loss at suction
Go
Verified
Pressure loss coefficient at inlet of duct
Go
Verified
Pressure loss coefficient at outlet of duct
Go
Verified
Pressure Loss due to Gradual Contraction given Pressure Loss Coefficient at Section 1
Go
Verified
Pressure Loss due to Gradual Contraction given Velocity of air at point 2
Go
Verified
Pressure Loss due to sudden Contraction given Velocity of Air at point 1
Go
Verified
Pressure Loss due to sudden Contraction given Velocity of Air at point 2
Go
Verified
Pressure loss due to sudden enlargement
Go
Dynamics
(1)
Verified
Angle of banking
Go
4 More Dynamics Calculators
Go
Dynamometer
(19)
Created
Constant for particular shaft for torsion dynamometer
Go
Created
Distance moved in one revolution by rope brake dynamometer
Go
Created
Load on Brake for Rope Brake Dynamometer
Go
Created
Polar moment of inertia of shaft for hollow shaft for torsion dynamometer
Go
Created
Polar moment of inertia of shaft for solid shaft for torsion dynamometer
Go
Created
Polar moment of inertia of shaft for torsion dynamometer
Go
Created
Power Transmitted by Torsion Dynamometer
Go
Created
Power Transmitted for Epicyclic-train Dynamometer
Go
Created
Power Transmitted for Epicyclic-train Dynamometer using Tangential Effort
Go
Created
Tangential effort for epicyclic-train dynamometer
Go
Created
Tension in slack side of belt for belt transmission dynamometer
Go
Created
Tension in tight side of belt for belt transmission dynamometer
Go
Created
Torque Acting on Shaft for Torsion Dynamometer
Go
Created
Torque on Shaft of Prony Brake Dynamometer
Go
Created
Torque on Shaft of Prony Brake Dynamometer using Radius of Pulley
Go
Created
Torque Transmitted for Epicyclic Train Dynamometer
Go
Created
Torque transmitted if power is known for epicyclic-train dynamometer
Go
Created
Torsion equation for torsion dynamometer
Go
Created
Torsion Equation for Torsion Dynamometer using Modulus of Rigidity
Go
Eccentrically Loaded Bolted Joints in Shear
(3)
Verified
Imaginary Force at Center of Gravity of Bolted Joint given Primary Shear Force
Go
Verified
Number of Bolts given Primary Shear Force
Go
Verified
Primary Shear Force of Eccentrically Loaded Bolted Connection
Go
Eccentricity
(5)
Verified
Eccentricity of Bearing in Terms of Minimum Film Thickness
Go
Verified
Eccentricity of Bearing in Terms of Radial Clearance and Eccentricity
Go
Verified
Eccentricity Ratio in Terms of Minimum Film Thickness of Bearing
Go
Verified
Eccentricity Ratio of Bearing in Terms of Minimum Film Thickness Variable
Go
Verified
Eccentricity Ratio of Bearing in Terms of Radial Clearance and Eccentricity
Go
Effect of Inertia of the Constraint on Torsional Vibrations
(8)
Created
Angular velocity of element
Go
Created
Angular Velocity of Free End using Kinetic Energy of Constraint
Go
Created
Kinetic Energy possessed by Element
Go
Created
Mass Moment of Inertia of Element
Go
Created
Natural frequency of torsional vibration due to effect of inertia of constraint
Go
Created
Torsional stiffness of shaft due to effect of constraint on torsional vibrations
Go
Created
Total kinetic energy of constraint
Go
Created
Total Mass Moment of Inertia of Constraint given Kinetic Energy of Constraint
Go
Effect of Internal Pressure on Dimension of Thin Cylindrical Shell
(23)
Created
Diameter of cylindrical shell given change in length of cylindrical shell
Go
Created
Diameter of thin cylindrical shell given volumetric strain
Go
Created
Diameter of thin cylindrical strain given volumetric strain
Go
Created
Hoop stress given circumferential strain
Go
Created
Hoop stress in thin cylindrical vessel given Longitudinal strain
Go
Created
Internal diameter of thin cylindrical vessel given circumferential strain
Go
Created
Internal diameter of thin cylindrical vessel given longitudinal strain
Go
Created
Internal fluid pressure given change in length of cylindrical shell
Go
Created
Internal fluid pressure given circumferential strain
Go
Created
Internal fluid pressure in shell given volumetric strain
Go
Created
Internal fluid pressure in thin cylindrical vessel given change in diameter
Go
Created
Internal fluid pressure in thin cylindrical vessel given longitudinal strain
Go
Created
Length of cylindrical shell given change in length of cylindrical shell
Go
Created
Length of cylindrical shell given change in volume of cylindrical shell
Go
Created
Length of thin cylindrical strain given volumetric strain
Go
Created
Longitudinal stress given circumferential strain
Go
Created
Longitudinal stress in thin cylindrical vessel given Longitudinal strain
Go
Created
Original circumference of thin cylindrical vessel given circumferential strain
Go
Created
Original diameter of thin cylindrical vessel given circumferential strain
Go
Created
Original diameter of vessel given change in diameter
Go
Created
Original length of vessel given longitudinal strain
Go
Created
Original volume of cylindrical shell given volumetric strain
Go
Created
Volume of thin cylindrical shell given circumferential and longitudinal strain
Go
Effective angle of attack
(3)
Verified
Effective angle of attack of finite wing
Go
Verified
Geometric angle of attack given effective angle of attack
Go
Verified
Induced angle of attack given effective angle of attack
Go
Effective Length Of A Column
(20)
Created
Crippling load for any type of end condition
Go
Created
Crippling load given crippling stress
Go
Created
Crippling load given effective length and radius of gyration
Go
Created
Crippling stress
Go
Created
Crippling stress given crippling load
Go
Created
Cross sectional area of column given effective length and radius of gyration
Go
Created
Cross-sectional area of column given crippling stress
Go
Created
Effective length given crippling load and radius of gyration
Go
Created
Effective length of column given actual length if both ends of column are fixed
Go
Created
Effective length of column given actual length if one end is fixed other is free
Go
Created
Effective length of column given actual length if one end is fixed other is hinged
Go
Created
Effective length of column given crippling load for any type of end condition
Go
Created
Effective length of column given crippling stress
Go
Created
Least radius of gyration given slenderness ratio
Go
Created
Modulus of elasticity given crippling load for any type of end condition
Go
Created
Modulus of elasticity given effective length and radius of gyration
Go
Created
Modulus of elasticity of column given crippling stress
Go
Created
Moment of inertia given crippling load for any type of end condition
Go
Created
Radius of gyration given crippling stress
Go
Created
Radius of gyration given effective length and crippling load
Go
Effective Load on Gear Tooth
(2)
Verified
Dynamic load on Gear
Go
Verified
Tolerance factor of Gear
Go
11 More Effective Load on Gear Tooth Calculators
Go
Effective Thermal Conductivity and Heat Transfer
(3)
Verified
Effective thermal conductivity for annular space between concentric cylinders
Go
Verified
Effective thermal conductivity given Prandtl number
Go
Verified
Heat transfer per unit length for annular space between concentric cylinders
Go
5 More Effective Thermal Conductivity and Heat Transfer Calculators
Go
Effectiveness
(3)
Verified
Effectiveness of double pipe counter flow heat exchanger given C equal to 1
Go
Verified
Effectiveness when mc-cc is minimum value
Go
Verified
Effectiveness when mhch is minimum value
Go
9 More Effectiveness Calculators
Go
Efficiency of Heating and Cooling coil
(4)
Verified
Efficiency of cooling coil
Go
Verified
Efficiency of cooling coil given by-pass factor
Go
Verified
Efficiency of heating coil
Go
Verified
Efficiency of heating coil given by-pass factor
Go
Efficiency of Longitudinal and Circumferential Joint
(10)
Created
Efficiency of circumferential joint given longitudinal stress
Go
Created
Efficiency of longitudinal joint given hoop stress
Go
Created
Hoop stress given efficiency of longitudinal joint
Go
Created
Internal diameter of vessel given hoop stress and efficiency of longitudinal joint
Go
Created
Internal diameter of vessel given longitudinal stress and efficiency of circumferential joint
Go
Created
Internal fluid pressure given longitudinal stress and efficiency of circumferential joint
Go