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Calculators Created by Dipto Mandal
Dipto Mandal
Indian Institute of Information Technology
(IIIT)
,
Guwahati
46
Formulas Created
371
Formulas Verified
59
Across Categories
List of Calculators by Dipto Mandal
Following is a combined list of all the calculators that have been created and verified by Dipto Mandal. Dipto Mandal has created 46 and verified 371 calculators across 59 different categories till date.
Values of load for the various types of beams and under various load conditions.
(8)
Verified
Eccentric Point Load for Fixed Beam
Go
Verified
Eccentric Point Load for Simply Supported Beam
Go
Verified
Value of load for Cantilever beam with point load at free end
Go
Verified
Value of load for Cantilever beam with uniformly distributed load
Go
Verified
Value of load for fixed beam with central point load
Go
Verified
Value of load for fixed beam with uniformly distributed load
Go
Verified
Value of load for simply supported beam with central point load
Go
Verified
Value of load for simply supported beam with uniformly distributed load
Go
Angular Frequency
(3)
Created
Angular frequency given constant K and mass
Go
Created
Angular frequency given velocity and distance A
Go
Created
Angular frequency of shm
Go
Arithmetic Mean
(2)
Verified
Arithmetic Mean given Geometric and Harmonic Means
Go
Verified
Arithmetic Mean given Two Numbers
Go
1 More Arithmetic Mean Calculators
Go
Atom
(1)
Verified
Energy in nth Bohr's Orbit
Go
9 More Atom Calculators
Go
Basics
(1)
Verified
Isobaric Work for given pressure and volumes
Go
11 More Basics Calculators
Go
Brake
(3)
Verified
Tension in Band between First and Second block for Band and Block Brake
Go
Verified
Tension in tight side for band and block brake
Go
Verified
Tension in Tight Side of Band for Simple Band Brake given Permissible Tensile Stress
Go
2 More Brake Calculators
Go
Braking Torque
(4)
Verified
Braking torque for band and block brake, considering thickness of band
Go
Verified
Braking torque for band and block brake, Neglecting thickness of band
Go
Verified
Braking Torque on Drum for Simple Band Brake considering Band Thickness
Go
Verified
Braking torque on drum for simple band brake, neglecting thickness of band
Go
8 More Braking Torque Calculators
Go
Circular Section
(19)
Verified
Average shear force for circular section
Go
Verified
Average shear stress for circular section
Go
Verified
Average Shear Stress for Circular Section using Maximum Shear Stress
Go
Verified
Maximum Shear Force using Radius of Circular Section
Go
Verified
Maximum shear stress for circular section
Go
Verified
Maximum Shear Stress for Circular Section using Average Shear Stress
Go
Verified
Maximum Shear Stress using Radius of Circular Section
Go
Verified
Moment of inertia of circular section
Go
Verified
Moment of Inertia of Circular Section given Shear Stress
Go
Verified
Moment of Inertia of Circular Section using Maximum Shear Stress
Go
Verified
Moment of Shaded Area (area above considered layer) about Neutral Axis
Go
Verified
Radius of Circular Section given Width of Beam at Considered Level
Go
Verified
Radius of Circular Section using Average Shear Stress
Go
Verified
Radius of Circular Section using Maximum Shear Stress
Go
Verified
Shear force distribution for circular section
Go
Verified
Shear Force using Maximum Shear Stress
Go
Verified
Shear stress distribution for circular section
Go
Verified
Width of Beam at Considered Level using Radius of Circular Section
Go
Verified
Width of Beam at Considered Level using Shear Stress for Circular Section
Go
Circular Section
(6)
Verified
Diameter of circular section for given moment of inertia about neutral axis
Go
Verified
Diameter of circular section for given section modulus
Go
Verified
Diameter of Circular Section given Distance of Outermost Layer from Neutral Layer
Go
Verified
Distance of outermost layer from neutral layer in circular sections
Go
Verified
Moment of inertia about neutral axis for circular section
Go
Verified
Section modulus for circular section
Go
Critical or Whirling Speed of a Shaft
(11)
Verified
Additional Deflection of centre of Gravity of Rotor using Natural Circular Frequency
Go
Verified
Additional Deflection of centre of gravity of Rotor using whirling speed
Go
Verified
Additional deflection of centre of gravity of rotor when shaft starts rotating
Go
Verified
Critical or Whirling Speed given Static Deflection
Go
Verified
Critical or whirling Speed given Stiffness of Shaft
Go
Verified
Critical or Whirling speed in r.p.s
Go
Verified
Force Resisting Additional Deflection of Centre of Gravity of Rotor
Go
Verified
Mass of Rotor given Centrifugal Force
Go
Verified
Natural circular frequency of shaft
Go
Verified
Static deflection of shaft
Go
Verified
Stiffness of shaft for equilibrium position
Go
1 More Critical or Whirling Speed of a Shaft Calculators
Go
Distance
(4)
Created
Distance from start given restoring force and constant k
Go
Created
Distance traveled by particle in shm when velocity becomes zero
Go
Created
Distance traveled given velocity
Go
Created
Distance traveled in SHM given angular frequency
Go
Effect of Inertia of the Constraint on Torsional Vibrations
(8)
Verified
Angular velocity of element
Go
Verified
Angular Velocity of Free End using Kinetic Energy of Constraint
Go
Verified
Kinetic Energy possessed by Element
Go
Verified
Mass Moment of Inertia of Element
Go
Verified
Natural frequency of torsional vibration due to effect of inertia of constraint
Go
Verified
Torsional stiffness of shaft due to effect of constraint on torsional vibrations
Go
Verified
Total kinetic energy of constraint
Go
Verified
Total Mass Moment of Inertia of Constraint given Kinetic Energy of Constraint
Go
Elasticity & Simple Harmonic Motion(SHM)
(23)
Created
Accelaration given constant K and distance traveled
Go
Created
Acceleration in SHM given angular frequency
Go
Created
Area of body given stress
Go
Created
Change in length given longitudinal stress
Go
Created
Change in volume of body given volumetric strain
Go
Created
Displacement of upper surface
Go
Created
Frequency of SHM
Go
Created
Mass of body given distance traveled and constant k
Go
Created
Mass of particle given angular frequency
Go
Created
Normal stress or longitudinal stress
Go
Created
Original length given longitudinal stress
Go
Created
Original volume of body given volumetric strain
Go
Created
Perpendicular distance between two surfaces
Go
Created
Phase in SHM
Go
Created
Ratio of shear
Go
Created
Restoring force given stress
Go
Created
Restoring force in shm
Go
Created
Square of different distances traveled in SHM
Go
Created
Time Period of SHM
Go
Created
Total distance traveled given velocity and angular frequency
Go
Created
Velocity of particle in shm
Go
Created
Volume strain
Go
Created
Young's modulus of elasticity
Go
Elevation in Boiling Point
(2)
Verified
Boiling Point Elevation
Go
Verified
Molal Boiling Point Elevation Constant given Boiling Point Elevation
Go
22 More Elevation in Boiling Point Calculators
Go
Empirical Constant's For SHM
(3)
Created
Constant A given position
Go
Created
Constant k given angular frequency
Go
Created
Constant k given restoring force
Go
Finite Geometric Progression
(1)
Created
Common Ratio of Finite Geometric Progression
Go
1 More Finite Geometric Progression Calculators
Go
Force
(2)
Verified
Force on lever of simple band brake for anticlockwise rotation of drum
Go
Verified
Force on lever of simple band brake for clockwise rotation of drum
Go
13 More Force Calculators
Go
Free Torsional Vibrations of a Single Rotor System
(2)
Verified
Modulus of rigidity of shaft for free torsional vibration of single rotor system
Go
Verified
Natural frequency of free torsional vibration of single rotor system
Go
Free Torsional Vibrations of a Two Rotor System
(6)
Verified
Distance of node from rotor A, for torsional vibration of two rotor system
Go
Verified
Distance of node from rotor B, for torsional vibration of two rotor system
Go
Verified
Mass moment of inertia of rotor A, for torsional vibration of two rotor system
Go
Verified
Mass moment of inertia of rotor B, for torsional vibration of two rotor system
Go
Verified
Natural frequency of free torsional vibration for rotor A of two rotor system
Go
Verified
Natural frequency of free torsional vibration for rotor B of two rotor system
Go
Frequency of Free Damped Vibrations
(19)
Verified
Amplitude reduction factor
Go
Verified
Circular damped frequency (under damping)
Go
Verified
Circular Damped Frequency given Natural Frequency (underdamping)
Go
Verified
Condition for critical damping
Go
Verified
Critical damping coefficient
Go
Verified
Damping factor
Go
Verified
Damping factor(in terms of natural frequency)
Go
Verified
Displacement of mass from mean position for under damping condition
Go
Verified
Frequency constant for damped vibrations (underdamping)
Go
Verified
Frequency constant for damped vibrations if circular frequency is known(underdamping)
Go
Verified
Frequency of damped vibration (under damping)
Go
Verified
Frequency of Damped Vibration using Natural Frequency (underdamping)
Go
Verified
Frequency of Undamped Vibration using under damping
Go
Verified
Logarithmic decrement
Go
Verified
Logarithmic Decrement using Circular Damped Frequency
Go
Verified
Logarithmic Decrement using Circular Damping Coefficient
Go
Verified
Logarithmic Decrement using Natural Frequency
Go
Verified
Periodic time of vibration (under damping)
Go
Verified
Periodic Time of Vibration using Natural Frequency (underdamping)
Go
Frequency of Under Damped Forced Vibrations
(15)
Verified
Complementary function
Go
Verified
Damping coefficient
Go
Verified
Deflection of system under static force
Go
Verified
External periodic disturbing force
Go
Verified
Maximum Displacement of Forced Vibration
Go
Verified
Maximum Displacement of Forced Vibration at Resonance
Go
Verified
Maximum Displacement of Forced Vibration using Natural Frequency
Go
Verified
Maximum Displacement of Forced Vibration with Negligible Damping
Go
Verified
Particular integral
Go
Verified
Phase constant
Go
Verified
Static force
Go
Verified
Static Force using Maximum Displacement or Amplitude of Forced Vibration
Go
Verified
Static force when damping is negligible
Go
Verified
Total displacement of forced vibration given particular integral and complementary function
Go
Verified
Total displacement of forced vibrations
Go
Harmonic Progression
(1)
Created
Sum of First N Terms of Harmonic Progression
Go
1 More Harmonic Progression Calculators
Go
Heat Transfer
(1)
Verified
Heat Transfer by Conduction at Base
Go
17 More Heat Transfer Calculators
Go
Hexagonal Pyramid
(1)
Verified
Volume of Hexagonal Pyramid
Go
2 More Hexagonal Pyramid Calculators
Go
Hollow Circular Section
(5)
Verified
Distance of outermost layer from neutral axis in hollow circular section
Go
Verified
Inner Diameter of Hollow Circular Section given Section Modulus
Go
Verified
Moment of inertia of hollow circular section
Go
Verified
Outer diameter of hollow circular section
Go
Verified
Section modulus of hollow circular section
Go
Hollow Rectangular Section
(5)
Verified
Distance of outer most layer from neutral axis for hollow rectangular section
Go
Verified
Moment of inertia for hollow rectangular section
Go
Verified
Outer Breadth of Hollow Rectangular Section given Section Modulus
Go
Verified
Outer length of hollow rectangular section
Go
Verified
Section modulus for hollow rectangular section
Go
Intoduction
(5)
Created
Decay of current in LR circuit
Go
Created
Growth of Current in LR Circuit
Go
Created
Self Inductance of Solenoid
Go
Created
Time Constant of LR Circuit
Go
Created
Total flux in self inductance
Go
10 More Intoduction Calculators
Go
Inverse Trigonometric
(3)
Verified
Value of 2 ArcTan A
Go
Verified
Value of 3 ArcTan A
Go
Verified
Value of ArcSec A given ArcCosec A
Go
3 More Inverse Trigonometric Calculators
Go
Longitudinal vibration
(6)
Verified
Length of constraint for longitudinal vibration
Go
Verified
Longitudinal velocity of free end for longitudinal vibration
Go
Verified
Natural frequency of longitudinal vibration
Go
Verified
Total Kinetic Energy of Constraint in Longitudinal Vibration
Go
Verified
Total mass of constraint for longitudinal vibration
Go
Verified
Velocity of small element for longitudinal vibration
Go
Magnification Factor or Dynamic Magnifier
(6)
Verified
Magnification factor
Go
Verified
Magnification factor at resonance
Go
Verified
Magnification Factor given Displacement of Vibrations
Go
Verified
Magnification factor if there is no damping
Go
Verified
Maximum Displacement given Magnification Factor
Go
Verified
Natural Circular Frequency given Magnification Factor
Go
Natural Frequency of Free Torsional Vibrations
(13)
Verified
Accelerating force
Go
Verified
Angular displacement of shaft from mean position
Go
Verified
Angular velocity of shaft
Go
Verified
Moment of Inertia of Disc given Angular Velocity
Go
Verified
Moment of Inertia of Disc given Time Period of Vibration
Go
Verified
Moment of Inertia of Disc using Natural Frequency of Vibration
Go
Verified
Natural frequency of vibration
Go
Verified
Restoring force for free torsional vibrations
Go
Verified
Time Period for Vibrations
Go
Verified
Torsional stiffness of shaft
Go
Verified
Torsional Stiffness of Shaft given Angular Velocity
Go
Verified
Torsional Stiffness of Shaft given Natural Frequency of Vibration
Go
Verified
Torsional Stiffness of Shaft given Time Period of Vibration
Go
Natural Frequency of Free Transverse Vibrations
(8)
Verified
Acceleration of Body given Stiffness of Shaft
Go
Verified
Length of shaft
Go
Verified
Load at Free End in Free Transverse Vibrations
Go
Verified
Moment of Inertia of Shaft given Static Deflection
Go
Verified
Natural Frequency of free transverse vibrations
Go
Verified
Restoring Force using Stiffness of Shaft
Go
Verified
Static Deflection given Moment of Inertia of Shaft
Go
Verified
Time period of free transverse vibrations
Go
Natural Frequency of Free Transverse Vibrations Due to Uniformly Distributed Load Acting Over a Simply Supported Shaft
(17)
Verified
Circular frequency due to uniformly distributed load
Go
Verified
Circular Frequency given Static Deflection
Go
Verified
Length of Shaft given Circular Frequency
Go
Verified
Length of Shaft given Natural Frequency
Go
Verified
Length of Shaft given Static Deflection
Go
Verified
Maximum bending moment at distance x from end A
Go
Verified
Moment of Inertia of Shaft given Circular Frequency
Go
Verified
Moment of Inertia of Shaft given Natural Frequency
Go
Verified
Moment of Inertia of shaft given static deflection given load per unit length
Go
Verified
Natural frequency due to uniformly distributed load
Go
Verified
Natural Frequency given Static Deflection
Go
Verified
Static deflection at distance x from end A
Go
Verified
Static deflection of simply supported shaft due to uniformly distributed load
Go
Verified
Static Deflection using Natural Frequency
Go
Verified
Uniformly Distributed Load Unit Length given Circular Frequency
Go
Verified
Uniformly Distributed Load Unit Length given Natural Frequency
Go
Verified
Uniformly Distributed Load Unit Length given Static Deflection
Go
Natural Frequency of Free Transverse Vibrations For a Shaft Subjected to a Number of Point Loads
(3)
Verified
Dunkerley's empirical formula, for natural frequency of whole system
Go
Verified
Natural frequency of transverse vibration due to point load
Go
Verified
Natural frequency of transverse vibration due to uniformly distributed load
Go
Natural Frequency of Free Transverse Vibrations of a Shaft Fixed at Both Ends Carrying a Uniformly Distributed Load
(17)
Verified
Bending Moment at some Distance from One End
Go
Verified
Circular frequency given static deflection (Shaft fixed, uniformly distributed load)
Go
Verified
Length of shaft given natural circular frequency (Shaft fixed, uniformly distributed load)
Go
Verified
Length of shaft given natural frequency (Shaft fixed, uniformly distributed load)
Go
Verified
Length of shaft in given static deflection (Shaft fixed, uniformly distributed load)
Go
Verified
Load given natural circular frequency (Shaft fixed, uniformly distributed load)
Go
Verified
Load given natural frequency for fixed shaft and uniformly distributed load
Go
Verified
Load using static deflection(Shaft fixed, uniformly distributed load)
Go
Verified
M.I of shaft given natural circular frequency (Shaft fixed, uniformly distributed load)
Go
Verified
M.I of shaft given natural frequency for fixed shaft and uniformly distributed load
Go
Verified
M.I of shaft given static deflection for fixed Shaft and uniformly distributed load
Go
Verified
Natural circular frequency of shaft fixed at both ends and carrying uniformly distributed load
Go
Verified
Natural frequency given static deflection (Shaft fixed, uniformly distributed load)
Go
Verified
Natural frequency of shaft fixed at both ends and carrying uniformly distributed load
Go
Verified
Static deflection at distance x from end A given length of shaft
Go
Verified
Static deflection given natural frequency (Shaft fixed, uniformly distributed load)
Go
Verified
Static deflection of shaft due to uniformly distributed load given length of shaft
Go
Pentagonal Pyramid
(1)
Verified
Lateral Surface Area of Pentagonal Pyramid
Go
2 More Pentagonal Pyramid Calculators
Go
Rectangular Section
(10)
Verified
Average Shear Stress for Rectangular Section
Go
Verified
Average Shear Stress given Maximum Shear Stress for Rectangular Section
Go
Verified
Distance of C.G of area(area above considered level)from neutral axis for rectangular section
Go
Verified
Distance of considered level from neutral axis for rectangular section
Go
Verified
Maximum Shear Stress for Rectangular Section
Go
Verified
Moment of inertia of rectangular section about neutral axis
Go
Verified
Shear force for rectangular section
Go
Verified
Shear force variation across neutral axis for rectangular section
Go
Verified
Shear stress for rectangular section
Go
Verified
Shear stress variation across neutral axis for rectangular section
Go
Rectangular Section
(5)
Verified
Breadth of Rectangular Section given Section Modulus
Go
Verified
Distance of outermost layer from neutral layer for rectangular section
Go
Verified
Length of Rectangular Section given Section Modulus
Go
Verified
Length of Rectangular Section using Distance of Outermost Layer from Neutral Layer
Go
Verified
Section modulus for rectangular section
Go
Rectangular Section Is Subjected To Load Eccentric To Both Axis
(10)
Verified
Bending stress due to eccentricity about y-y axis
Go
Verified
Bending stress due to eccentricity about y-y axis given Eccentric Load on Column
Go
Verified
Distance of Load point from x-axis given Bending Stress about x-x axis
Go
Verified
Distance of Load point from y-axis given Bending Stress about y-y axis
Go
Verified
Eccentric Load on Column given Bending Stress along x-x axis
Go
Verified
Eccentric Load on Column given Bending Stress along y-y axis
Go
Verified
Eccentricity of Load about y-y axis given Bending Stress about y-y axis
Go
Verified
Moment of Inertia about x-x axis given Bending Stress about x-x axis
Go
Verified
Moment of Inertia about y-y axis given Bending Stress about y-y axis
Go
Verified
Moment of Load about y-y Axis given Bending Stress about y-y Axis
Go
8 More Rectangular Section Is Subjected To Load Eccentric To Both Axis Calculators
Go
Rectangular Section Is Subjected To Eccentric Load
(21)
Verified
Bending Stress given Moment due to Load
Go
Verified
Bending Stress using Eccentric Load and Eccentricity
Go
Verified
Depth of Column using Bending Stress and Eccentric load
Go
Verified
Depth of Column using Bending Stress and Moment Due to Load
Go
Verified
Eccentric Load using Bending Stress
Go
Verified
Eccentric Load using Maximum Stress
Go
Verified
Eccentric Load using Minimum Stress
Go
Verified
Eccentricity for given moment due to eccentric load
Go
Verified
Eccentricity using Bending Stress
Go
Verified
Eccentricity using Maximum Stress
Go
Verified
Eccentricity using Minimum Stress
Go
Verified
Load given Moment due to Eccentric Load
Go
Verified
Maximum stress
Go
Verified
Maximum Stress given Eccentric Load and Eccentricity
Go
Verified
Minimum stress
Go
Verified
Minimum Stress using Eccentric Load and Eccentricity
Go
Verified
Moment due to eccentric load
Go
Verified
Moment Due to Load given Bending Stress
Go
Verified
Moment of inertia of column section about neutral axis
Go
Verified
Width of Column given Bending Stress and Moment due to Load
Go
Verified
Width of Column using Bending Stress and Eccentric load
Go
1 More Rectangular Section Is Subjected To Eccentric Load Calculators
Go
Retardation of the Vehicle
(2)
Verified
Retardation of vehicle if vehicle moves down plane if brakes are applied to rear wheels only
Go
Verified
Retardation of vehicle when vehicle moves on level track if brakes are applied to rear wheels
Go
7 More Retardation of the Vehicle Calculators
Go
Section Modulus
(10)
Verified
Distance of outermost layer from neutral axis given maximum moment of resistance
Go
Verified
Distance of Outermost Layer from Neutral Axis using Section Modulus
Go
Verified
Maximum moment of resistance
Go
Verified
Maximum Moment of Resistance given Section Modulus
Go
Verified
Maximum Stress given Maximum Moment of Resistance
Go
Verified
Maximum Stress given Maximum Moment of Resistance and Section Modulus
Go
Verified
Moment of Inertia about Neutral Axis given Section Modulus
Go
Verified
Moment of Inertia of Neutral axis given Maximum Moment of Resistance
Go
Verified
Section Modulus given Distance between Outermost and Neutral Layer
Go
Verified
Section Modulus given Maximum Moment of Resistance
Go
1 More Section Modulus Calculators
Go
Semiconductor
(1)
Created
Maximum Efficiency of Steam Engine(Semiconductors)
Go
11 More Semiconductor Calculators
Go
Shear Stress at a Section
(7)
Verified
Area of section above considered level
Go
Verified
Distance of center of gravity of area(above considered level) from neutral axis
Go
Verified
Moment of inertia of section about neutral axis
Go
Verified
Shear force at section
Go
Verified
Shear Force at Section given Shear Area
Go
Verified
Shear stress at section
Go
Verified
Width of beam at considered level
Go
Shear Stress Distribution in Flange
(15)
Verified
Area of Flange or Area above considered Section
Go
Verified
Distance of C.G of Area(area above considered section)of Flange from Neutral Axis
Go
Verified
Distance of considered section from neutral axis for given shear stress in flange
Go
Verified
Distance of considered Section from Neutral Axis for Lower Edge of Flange
Go
Verified
Distance of considered Section from Neutral Axis for Upper Edge of Flange
Go
Verified
Inner Length of I-section given Shear Stress for Lower Edge of Flange
Go
Verified
Moment of Inertia of I section given Shear Stress for Lower Edge of Flange
Go
Verified
Moment of inertia of section for I-section
Go
Verified
Outer Length of I section given Shear Stress for Lower Edge of Flange
Go
Verified
Outer Length of I-section given Shear Stress in Flange
Go
Verified
Shear force distribution in I-section for lower edge of flange
Go
Verified
Shear Force in Flange for I-section
Go
Verified
Shear stress distribution in I-section for lower edge of flange
Go
Verified
Shear Stress in Flange for I-section
Go
Verified
Width of Section given Area above considered Section of Flange
Go
Shear Stress Distribution in Web
(16)
Verified
Distance of considered level from neutral axis at junction of top of web
Go
Verified
Maximum shear force at neutral axis
Go
Verified
Maximum shear stress at neutral axis
Go
Verified
Moment of flanged area about neutral axis
Go
Verified
Moment of Inertia of Section given Maximum Shear Stress and Force
Go
Verified
Moment of Inertia of Section given Shear Stress at Junction of Top of Web
Go
Verified
Moment of Inertia of Section using Shear Stress of Web
Go
Verified
Moment of shaded area of web about neutral axis
Go
Verified
Shear force at junction of top of web
Go
Verified
Shear Force in Web
Go
Verified
Shear stress at junction of top of web
Go
Verified
Shear Stress in Web
Go
Verified
Thickness of Web given Maximum Shear Stress and Force
Go
Verified
Thickness of Web using Shear Stress of Web
Go
Verified
Width of Section given Moment of Flange Area about Neutral Axis
Go
Verified
Width of Section given Shear Stress at Junction of Top of Web
Go
2 More Shear Stress Distribution in Web Calculators
Go
Strain Energy Stored In A Body Due To Shear Stress
(8)
Verified
Average Load Value given Work done by gradually applied Shear Force
Go
Verified
Shear Strain Produced given work done by gradually applied Shear Force
Go
Verified
Shear Stress produced given Strain Energy stored in body due to Shear Stress
Go
Verified
Shear Stress Produced given work done by gradually applied Shear Force
Go
Verified
Strain energy stored in body due to shear stress
Go
Verified
Work Done by Gradually Applied Shear Force given Average Load
Go
Verified
Work Done by Gradually Applied Shear Force given Shear Strain
Go
Verified
Work done by gradually applied Shear Force given Shear Stress
Go
Strain Energy Stored In A Body When The Load Is Applied With Impact
(10)
Verified
Cross Sectional Area of Rod using Stress Induced in Rod due to Impact Load
Go
Verified
Height through which load is dropped given stress induced in rod due to impact load
Go
Verified
Height through which Load is dropped using Work done by Load
Go
Verified
Length of Rod given Stress Induced in Rod due to Impact Load
Go
Verified
Load Dropped given Stress Induced in Rod due to Impact Load
Go
Verified
Stress induced in rod due to impact load
Go
Verified
Stress induced in rod due to impact load if height through which load dropped is zero
Go
Verified
Value of Load Applied with Impact given Work Done by Load
Go
Verified
Value of load dropped if height through which load dropped is zero
Go
Verified
Work Done by Load for Small Extension of Rod
Go
Stress Variation
(18)
Verified
Distance between Neutral and Considered layer in Beam
Go
Verified
Distance between Neutral and Considered Layer using Moment of Resistance
Go
Verified
Distance between Neutral and Considered Layers in Beams
Go
Verified
Force on Layer at Distance from Neutral Layer of Beam
Go
Verified
Force on Layer of Beams given Stress in Layer
Go
Verified
Moment of Inertia of Area of Section given Young's Modulus of Beam
Go
Verified
Moment of Inertia of Area of Section of Beam given Stress in Layer
Go
Verified
Moment of resistance
Go
Verified
Moment of Resistance using Stress in Layer of Beam
Go
Verified
Radius of Neutral Axis using Moment of Resistance
Go
Verified
Radius of neutral layer
Go
Verified
Radius of Neutral Layer given Force on Considered Layer
Go
Verified
Stress in layer if it's considered that beam is subjected to simple bending
Go
Verified
Stress in Layer of Beam given Force on Layer
Go
Verified
Stress in Layer of Beam given Moment of Resistance
Go
Verified
Young's modulus of beam
Go
Verified
Young's Modulus of Beam given Force on Layer
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Verified
Young's Modulus of Beam using Moment of Resistance
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Sum of 4th Powers
(1)
Created
Sum of 4th Powers of First N Natural Numbers
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Sum of First N Terms of Arithmetic Progression
(1)
Verified
Sum of First N Terms of Arithmetic Progression
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1 More Sum of First N Terms of Arithmetic Progression Calculators
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Sum of Squares
(2)
Created
Sum of Squares of First N Even Natural Numbers
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Created
Sum of Squares of First N Odd Natural Numbers
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1 More Sum of Squares Calculators
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Theoretical Vapour compression cycle with Dry Saturated vapour after compression
(1)
Verified
Refrigerating Effect(for given h1 and h4)
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8 More Theoretical Vapour compression cycle with Dry Saturated vapour after compression Calculators
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Total Normal Reaction
(2)
Verified
Total normal reaction between ground and front wheels for 0 accln, brakes applied to rear wheels
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Verified
Total normal reaction between ground and rear wheels for 0 accln, brakes applied to rear wheels
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10 More Total Normal Reaction Calculators
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Transverse vibration
(6)
Verified
Length of constraint for transverse vibrations
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Verified
Natural frequency of transverse vibration
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Verified
Total kinetic energy of constraint for transverse vibrations
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Verified
Total mass of constraint for transverse vibrations
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Verified
Transverse velocity of free end
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Verified
Velocity of small element for transverse vibrations
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Trigonometric Formulas
(2)
Created
Cos 2A given Angle A
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Created
Sin 2A given Angle A
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3 More Trigonometric Formulas Calculators
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Values of length of beam for the various types of beams and under various load conditions
(8)
Verified
Length of beam for cantilever beam with point load at free end
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Verified
Length of beam for cantilever beam with uniformly distributed load
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Verified
Length of beam for fixed beam with central point load
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Verified
Length of beam for fixed beam with uniformly distributed load
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Verified
Length of beam for simply supported beam with central point load
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Verified
Length of beam for Simply supported beam with uniformly distributed load
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Verified
Length of Fixed Beam with Eccentric Point Load
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Verified
Length of Simply Supported Beam with Eccentric Point Load
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Values of static deflection for the various types of beams and under various load conditions
(8)
Verified
Static deflection for cantilever beam with point load at free end
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Verified
Static deflection for cantilever beam with uniformly distributed load
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Verified
Static deflection for fixed beam with central point load
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Verified
Static deflection for fixed beam with uniformly distributed point load
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Static deflection for simply supported beam with central point load
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Verified
Static Deflection for Simply Supported Beam with Eccentric Point Load
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Verified
Static deflection for simply supported beam with uniformly distributed load
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Verified
Static Deflection in Fixed Beam with Eccentric Point Load
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Vibration Isolation and Transmissibility
(18)
Verified
Angular Velocity of Vibration using Force Transmitted
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Verified
Applied force given transmissibility ratio
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Verified
Applied force given transmissibility ratio and maximum displacement of vibration
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Verified
Damping Coefficient using Force Transmitted
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Verified
Force transmitted
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Verified
Magnification factor given transmissibility ratio
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Verified
Magnification factor given transmissibility ratio given natural circular frequency
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Verified
Maximum displacement of vibration given Transmissibility ratio
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Verified
Maximum Displacement of Vibration using Force Transmitted
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Verified
Natural Circular Frequency given Transmissibility Ratio
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Verified
Stiffness of Spring using Force Transmitted
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Verified
Transmissibility ratio
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Verified
Transmissibility ratio given force transmitted
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Verified
Transmissibility Ratio given Magnification Factor
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Verified
Transmissibility ratio given natural circular frequency and critical damping coefficient
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Verified
Transmissibility ratio given natural circular frequency and magnification factor
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Verified
Transmissibility ratio if there is no damping
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Verified
Transmitted force given transmissibility ratio
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