Calculators Created by Dipto Mandal

Indian Institute of Information Technology (IIIT), Guwahati
45
Formulas Created
371
Formulas Verified
64
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 45 and verified 371 calculators across 64 different categories till date.
Verified Heat Transfer by Conduction at Base
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12 More Conduction, Convection and Radiation Calculators
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Verified Eccentric Point Load for Fixed Beam
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Verified Eccentric Point Load for Simply Supported Beam
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Verified Value of Load for Cantilever Beam with Point Load at Free End
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Verified Value of Load for Cantilever Beam with Uniformly Distributed Load
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Verified Value of Load for Fixed Beam with Central Point Load
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Verified Value of Load for Fixed Beam with Uniformly Distributed Load
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Verified Value of Load for Simply Supported Beam with Central Point Load
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Verified Value of Load for Simply Supported Beam with Uniformly Distributed Load
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Verified Arithmetic Mean given Geometric and Harmonic Means
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Verified Arithmetic Mean of Two Numbers
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4 More Arithmetic Mean Calculators
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Verified Energy in Nth Bohr's Orbit
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9 More Atomic Structure Calculators
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Verified Average Shear Force for Circular Section
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Verified Average Shear Stress for Circular Section
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Verified Average Shear Stress for Circular Section given Maximum Shear Stress
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Verified Shear Force in Circular Section
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Verified Shear Force using Maximum Shear Stress
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Verified Shear Stress Distribution for Circular Section
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Created Amplitude given Position
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Created Angular Frequency given Constant K and Mass
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Created Angular Frequency given Velocity and Distance
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Created Angular Frequency in SHM
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Created Frequency of SHM
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Created Mass of Particle given Angular Frequency
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Created Position of Particle in SHM
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Created Time Period of SHM
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Created Decay of Current in LR circuit
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Created Growth of Current in LR Circuit
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Created Self Inductance of Solenoid
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Created Time Constant of LR Circuit
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Created Total Flux in Self Inductance
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10 More Basics of Electromagentic Induction Calculators
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Brake (3)
Verified Tension in Band between First and Second Block for Band and Block Brake
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Verified Tension in Tight Side for Band and Block Brake
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Verified Tension in Tight Side of Band for Simple Band Brake given Permissible Tensile Stress
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2 More Brake Calculators
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Verified Braking Torque for Band and Block Brake, Considering Thickness of Band
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Verified Braking Torque for Band and Block Brake, Neglecting Thickness of Band
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Verified Braking Torque on Drum for Simple Band Brake Considering Band Thickness
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Verified Braking Torque on Drum for Simple Band Brake, Neglecting Thickness of Band
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8 More Braking Torque Calculators
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Verified Diameter of Circular Section given Distance of Outermost Layer from Neutral Layer
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Verified Diameter of Circular Section given Moment of Inertia about Neutral Axis
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Verified Diameter of Circular Section given Section Modulus
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Verified Distance of Outermost Layer from Neutral Layer in Circular Sections
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Verified Moment of Inertia about Neutral Axis for Circular Section
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Verified Section Modulus for Circular Section
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Verified Isobaric Work for given Pressure and Volumes
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8 More Closed System Work Calculators
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Created Common Ratio of Geometric Progression
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2 More Common Ratio of Geometric Progression Calculators
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Verified Additional Deflection of Centre of Gravity of Rotor using Natural Circular Frequency
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Verified Additional Deflection of Centre of Gravity of Rotor using Whirling Speed
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Verified Additional Deflection of Centre of Gravity of Rotor when Shaft Starts Rotating
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Verified Critical or Whirling Speed given Static Deflection
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Verified Critical or Whirling Speed given Stiffness of Shaft
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Verified Critical or Whirling Speed in R.P.S
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Verified Force Resisting Additional Deflection of Centre of Gravity of Rotor
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Verified Mass of Rotor given Centrifugal Force
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Verified Natural Circular Frequency of Shaft
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Verified Static Deflection of Shaft
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Verified Stiffness of Shaft for Equilibrium Position
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1 More Critical or Whirling Speed of Shaft Calculators
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Created Cos 2A
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Created Sin 2A
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8 More Double Angle Trigonometry Identities Calculators
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Verified Angular Velocity of Element
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Verified Angular Velocity of Free End using Kinetic Energy of Constraint
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Verified Kinetic Energy Possessed by Element
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Verified Mass Moment of Inertia of Element
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Verified Natural Frequency of Torsional Vibration due to Effect of Inertia of Constraint
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Verified Torsional Stiffness of Shaft due to Effect of Constraint on Torsional Vibrations
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Verified Total Kinetic Energy of Constraint
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Verified Total Mass Moment of Inertia of Constraint given Kinetic Energy of Constraint
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Verified Boiling Point Elevation
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Verified Molal Boiling Point Elevation Constant given Boiling Point Elevation
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22 More Elevation in Boiling Point Calculators
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Verified Refrigerating Effect(for given h1 and h4)
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7 More Enthalpy of Vapour Compression Refrigeration Cycle Calculators
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Force (2)
Verified Force on Lever of Simple Band Brake for Anticlockwise Rotation of Drum
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Verified Force on Lever of Simple Band Brake for Clockwise Rotation of Drum
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13 More Force Calculators
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Created Acceleration given Constant K and Distance Traveled
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Created Acceleration in SHM given Angular Frequency
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Created Constant K given Angular Frequency
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Created Constant K given Restoring Force
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Created Mass of Body given Distance Traveled and Constant K
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Created Restoring Force given Stress
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Created Restoring Force in SHM
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Verified Modulus of Rigidity of Shaft for Free Torsional Vibration of Single Rotor System
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Verified Natural Frequency of Free Torsional Vibration of Single Rotor System
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Verified Distance of Node from Rotor A, for Torsional Vibration of Two Rotor System
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Verified Distance of Node from Rotor B, for Torsional Vibration of Two Rotor System
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Verified Mass Moment of Inertia of Rotor A, for Torsional Vibration of Two Rotor System
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Verified Mass Moment of Inertia of Rotor B, for Torsional Vibration of Two Rotor System
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Verified Natural Frequency of Free Torsional Vibration for Rotor A of Two Rotor System
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Verified Natural Frequency of Free Torsional Vibration for Rotor B of Two Rotor System
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Verified Amplitude Reduction Factor
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Verified Circular Damped Frequency
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Verified Circular Damped Frequency given Natural Frequency
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Verified Condition for Critical Damping
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Verified Critical Damping Coefficient
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Verified Damping Factor
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Verified Damping Factor given Natural Frequency
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Verified Displacement of Mass from Mean Position
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Verified Frequency Constant for Damped Vibrations
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Verified Frequency Constant for Damped Vibrations given Circular Frequency
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Verified Frequency of Damped Vibration
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Verified Frequency of Damped Vibration using Natural Frequency
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Verified Frequency of Undamped Vibration
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Verified Logarithmic Decrement
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Verified Logarithmic Decrement using Circular Damped Frequency
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Verified Logarithmic Decrement using Circular Damping Coefficient
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Verified Logarithmic Decrement using Natural Frequency
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Verified Periodic Time of Vibration
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Verified Periodic Time of Vibration using Natural Frequency
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Verified Complementary Function
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Verified Damping Coefficient
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Verified Deflection of System under Static Force
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Verified External Periodic Disturbing Force
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Verified Maximum Displacement of Forced Vibration
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Verified Maximum Displacement of Forced Vibration at Resonance
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Verified Maximum Displacement of Forced Vibration using Natural Frequency
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Verified Maximum Displacement of Forced Vibration with Negligible Damping
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Verified Particular Integral
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Verified Phase Constant
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Verified Static Force
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Verified Static Force using Maximum Displacement or Amplitude of Forced Vibration
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Verified Static Force when Damping is Negligible
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Verified Total Displacement of Forced Vibration given Particular Integral and Complementary Function
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Verified Total Displacement of Forced Vibrations
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Verified Acceleration of Body given Stiffness of Shaft
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Verified Length of Shaft
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Verified Load at Free End in Free Transverse Vibrations
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Verified Moment of Inertia of Shaft given Static Deflection
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Verified Natural Frequency of Free Transverse Vibrations
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Verified Restoring Force using Stiffness of Shaft
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Verified Static Deflection given Moment of Inertia of Shaft
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Verified Time Period of Free Transverse Vibrations
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Created Sum of First N Terms of Harmonic Progression
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5 More Harmonic Progression Calculators
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Verified Volume of Hexagonal Pyramid
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3 More Hexagonal Pyramid Calculators
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Verified Distance of Outermost Layer from Neutral Axis in Hollow Circular Section
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Verified Inner Diameter of Hollow Circular Section given Section Modulus
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Verified Moment of Inertia of Hollow Circular Section
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Verified Outer Diameter of Hollow Circular Section
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Verified Section Modulus of Hollow Circular Section
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Verified Distance of Outermost Layer from Neutral Axis for Hollow Rectangular Sections
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Verified Moment of Inertia for Hollow Rectangular Section
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Verified Outer Breadth of Hollow Rectangular Section given Section Modulus
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Verified Outer Length of Hollow Rectangular Section
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Verified Section Modulus for Hollow Rectangular Section
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Verified ArcSec A given ArcCosec A
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Verified ArcTan A
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Verified ArcTan A using ArcSin Function
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3 More Inverse Trigonometry Calculators
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Verified Length of Constraint for Longitudinal Vibration
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Verified Longitudinal Velocity of Free End for Longitudinal Vibration
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Verified Natural Frequency of Longitudinal Vibration
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Verified Total Kinetic Energy of Constraint in Longitudinal Vibration
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Verified Total Mass of Constraint for Longitudinal Vibration
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Verified Velocity of Small Element for Longitudinal Vibration
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Verified Magnification Factor
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Verified Magnification Factor at Resonance
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Verified Magnification Factor given Displacement of Vibrations
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Verified Magnification Factor if there is No Damping
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Verified Maximum Displacement given Magnification Factor
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Verified Natural Circular Frequency given Magnification Factor
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Verified Maximum Shear Force given Radius of Circular Section
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Verified Maximum Shear Stress for Circular Section
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Verified Maximum Shear Stress for Circular Section given Average Shear Stress
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Verified Maximum Shear Stress given Radius of Circular Section
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Created Young's Modulus of Elasticity
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1 More Modulus of Elasticity Calculators
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Verified Area Moment of Considered Area about Neutral Axis
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Verified Moment of Inertia of Circular Section
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Verified Moment of Inertia of Circular Section given Maximum Shear Stress
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Verified Moment of Inertia of Circular Section given Shear Stress
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Verified Accelerating Force
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Verified Angular Displacement of Shaft from Mean Position
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Verified Angular Velocity of Shaft
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Verified Moment of Inertia of Disc given Angular Velocity
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Verified Moment of Inertia of Disc given Time Period of Vibration
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Verified Moment of Inertia of Disc using Natural Frequency of Vibration
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Verified Natural Frequency of Vibration
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Verified Restoring Force for Free Torsional Vibrations
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Verified Time Period for Vibrations
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Verified Torsional Stiffness of Shaft
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Verified Torsional Stiffness of Shaft given Angular Velocity
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Verified Torsional Stiffness of Shaft given Natural Frequency of Vibration
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Verified Torsional Stiffness of Shaft given Time Period of Vibration
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Created Maximum Efficiency of Steam Engine
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20 More Others and Extra Calculators
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Verified Lateral Surface Area of Pentagonal Pyramid
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3 More Pentagonal Pyramid Calculators
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Verified Radius of Circular Section given Average Shear Stress
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Verified Radius of Circular Section given Maximum Shear Stress
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Verified Radius of Circular Section given Width of Beam at Considered Level
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Verified Width of Beam at Considered Level given Radius of Circular Section
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Verified Width of Beam at Considered Level given Shear Stress for Circular Section
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Verified Breadth of Rectangular Section given Section Modulus
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Verified Distance of Outermost Layer from Neutral Layer for Rectangular Section
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Verified Length of Rectangular Section given Section Modulus
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Verified Length of Rectangular Section using Distance of Outermost Layer from Neutral Layer
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Verified Section Modulus for Rectangular Section
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Verified Bending Stress given Moment due to Load
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Verified Bending Stress using Eccentric Load and Eccentricity
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Verified Depth of Column using Bending Stress and Eccentric Load
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Verified Depth of Column using Bending Stress and Moment Due to Load
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Verified Eccentric Load using Bending Stress
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Verified Eccentric Load using Maximum Stress
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Verified Eccentric Load using Minimum Stress
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Verified Eccentricity for given Moment due to Eccentric Load
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Verified Eccentricity using Bending Stress
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Verified Eccentricity using Maximum Stress
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Verified Eccentricity using Minimum Stress
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Verified Load given Moment due to Eccentric Load
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Verified Maximum Stress
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Verified Maximum Stress given Eccentric Load and Eccentricity
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Verified Minimum Stress
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Verified Minimum Stress using Eccentric Load and Eccentricity
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Verified Moment due to eccentric load
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Verified Moment Due to Load given Bending Stress
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Verified Moment of inertia of column section about neutral axis
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Verified Width of Column given Bending Stress and Moment due to Load
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Verified Width of Column using Bending Stress and Eccentric Load
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1 More Rectangular Section Is Subjected to Eccentric Load Calculators
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Verified Bending Stress due to Eccentricity about y-y Axis
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Verified Bending Stress due to Eccentricity about y-y Axis given Eccentric Load on Column
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Verified Distance of Load Point from x-Axis given Bending Stress about x-x Axis
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Verified Distance of Load point from y-Axis given Bending Stress about y-y Axis
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Verified Eccentric Load on Column given Bending Stress along x-x Axis
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Verified Eccentric Load on Column given Bending Stress along y-y Axis
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Verified Eccentricity of Load about y-y Axis given Bending Stress about y-y Axis
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Verified Moment of Inertia about x-x Axis given Bending Stress about x-x Axis
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Verified Moment of Inertia about y-y Axis given Bending Stress about y-y Axis
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Verified Moment of Load about y-y Axis given Bending Stress about y-y Axis
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8 More Rectangular Section is Subjected to Load Eccentric to Both Axis Calculators
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Verified Retardation of Vehicle if Vehicle Moves down Plane if Brakes are Applied to Rear Wheels only
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Verified Retardation of Vehicle when Vehicle Moves on Level Track if Brakes are Applied to Rear Wheels
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7 More Retardation of the Vehicle Calculators
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Verified Distance of Outermost Layer from Neutral Axis given Maximum Moment of Resistance
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Verified Distance of Outermost Layer from Neutral Axis using Section Modulus
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Verified Maximum Moment of Resistance
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Verified Maximum Moment of Resistance given Section Modulus
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Verified Maximum Stress given Maximum Moment of Resistance
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Verified Maximum Stress given Maximum Moment of Resistance and Section Modulus
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Verified Moment of Inertia about Neutral Axis given Section Modulus
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Verified Moment of Inertia of Neutral axis given Maximum Moment of Resistance
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Verified Section Modulus given Distance between Outermost and Neutral Layer
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Verified Section Modulus given Maximum Moment of Resistance
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1 More Section Modulus Calculators
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Verified Bending Moment at Some Distance from One End
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Verified Circular Frequency given Static Deflection (Shaft Fixed, Uniformly Distributed Load)
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Verified Length of Shaft given Natural Circular Frequency (Shaft Fixed, Uniformly Distributed Load)
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Verified Length of Shaft given Natural Frequency (Shaft Fixed, Uniformly Distributed Load)
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Verified Length of Shaft in given Static Deflection (Shaft Fixed, Uniformly Distributed Load)
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Verified Load given Natural Circular Frequency (Shaft Fixed, Uniformly Distributed Load)
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Verified Load given Natural Frequency for Fixed Shaft and Uniformly Distributed Load
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Verified Load using Static Deflection (Shaft Fixed, Uniformly Distributed Load)
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Verified M.I of Shaft given Natural Circular Frequency (Shaft Fixed, Uniformly Distributed Load)
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Verified M.I of Shaft given Natural Frequency for Fixed Shaft and Uniformly Distributed Load
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Verified M.I of Shaft given Static Deflection for Fixed Shaft and Uniformly Distributed Load
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Verified Natural Circular Frequency of Shaft Fixed at Both Ends and Carrying Uniformly Distributed Load
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Verified Natural Frequency given Static Deflection (Shaft Fixed, Uniformly Distributed Load)
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Verified Natural Frequency of Shaft Fixed at Both Ends and Carrying Uniformly Distributed Load
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Verified Static Deflection at Distance x from End A given Length of Shaft
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Verified Static Deflection given Natural Frequency (Shaft Fixed, Uniformly Distributed Load)
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Verified Static Deflection of Shaft due to Uniformly Distributed Load given Length of Shaft
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Verified Dunkerley's Empirical Formula, for Natural Frequency of Whole System
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Verified Natural Frequency of Transverse Vibration due to Point Load
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Verified Natural Frequency of Transverse Vibration due to Uniformly Distributed Load
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Verified Area of Section above Considered Level
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Verified Distance of Center of Gravity of Area (above Considered Level) from Neutral Axis
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Verified Moment of Inertia of Section about Neutral Axis
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Verified Shear Force at Section
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Verified Shear Force at Section given Shear Area
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Verified Shear Stress at Section
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Verified Width of Beam at Considered Level
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Verified Area of Flange or Area above Considered Section
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Verified Distance of CG of Considered Area of Flange from Neutral Axis in I Section
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Verified Distance of Considered Section from Neutral Axis given Shear Stress in Flange
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Verified Distance of Lower Edge of Flange from Neutral Axis
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Verified Distance of Upper Edge of Flange from Neutral Axis
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Verified Inner Depth of I-section given Shear Stress in Lower Edge of Flange
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Verified Moment of Inertia of I section given Shear Stress in Lower Edge of Flange
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Verified Moment of Inertia of Section for I-section
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Verified Outer Depth of I section given Shear Stress in Lower Edge of Flange
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Verified Outer Depth of I-section given Shear Stress in Flange
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Verified Shear Force in Flange of I-section
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Verified Shear Force in Lower Edge of Flange in I-section
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Verified Shear Stress in Flange of I-section
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Verified Shear Stress in Lower Edge of Flange of I-section
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Verified Width of Section given Area above Considered Section of Flange
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Verified Distance of Considered Level from Neutral Axis at Junction of Top of Web
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Verified Maximum Shear Force in I Section
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Verified Maximum Shear Stress in I Section
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Verified Moment of Flange Area about Neutral Axis
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Verified Moment of Inertia of I-Section given Maximum Shear Stress and Force
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Verified Moment of Inertia of I-Section given Shear Stress of Web
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Verified Moment of Inertia of Section given Shear Stress at Junction of Top of Web
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Verified Moment of Shaded Area of Web about Neutral Axis
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Verified Shear Force at Junction of Top of Web
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Verified Shear Force in Web
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Verified Shear Stress at Junction of Top of Web
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Verified Shear Stress in Web
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Verified Thickness of Web given Maximum Shear Stress and Force
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Verified Thickness of Web given Shear Stress of Web
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Verified Width of Section given Moment of Flange Area about Neutral Axis
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Verified Width of Section given Shear Stress at Junction of Top of Web
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2 More Shear Stress Distribution in Web Calculators
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Verified Average Shear Stress for Rectangular Section
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Verified Average Shear Stress given Maximum Shear Stress for Rectangular Section
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Verified Distance of C.G of Area (above Considered Level) from Neutral Axis for Rectangular Section
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Verified Distance of Considered Level from Neutral Axis for Rectangular Section
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Verified Maximum Shear Stress for Rectangular Section
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Verified Moment of Inertia of Rectangular Section about Neutral Axis
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Verified Shear Force for Rectangular Section
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Verified Shear Force Variation across Neutral Axis for Rectangular Section
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Verified Shear Stress for Rectangular Section
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Verified Shear Stress Variation across Neutral Axis for Rectangular Section
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Strain (5)
Created Change in Volume of Body given Volumetric Strain
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Created Displacement of Upper Surface
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Created Original Volume of Body given Volumetric Strain
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Created Perpendicular Distance between Two Surfaces given Shear Angle
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Created Volume Strain
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1 More Strain Calculators
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Verified Average Load Value given Work done by Gradually Applied Shear Force
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Verified Shear Strain Produced given Work Done by Gradually Applied Shear Force
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Verified Shear Stress Produced given Strain Energy Stored in Body Due to Shear Stress
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Verified Shear Stress Produced given Work Done by Gradually Applied Shear Force
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Verified Strain Energy Stored in Body due to Shear Stress
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Verified Work Done by Gradually Applied Shear Force given Average Load
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Verified Work Done by Gradually Applied Shear Force given Shear Strain
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Verified Work Done by Gradually Applied Shear Force given Shear Stress
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Verified Cross Sectional Area of Rod using Stress Induced in Rod due to Impact Load
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Verified Height through which Load is Dropped given Stress Induced in Rod due to Impact Load
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Verified Height through which Load is Dropped using Work done by Load
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Verified Length of Rod given Stress Induced in Rod due to Impact Load
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Verified Load Dropped given Stress Induced in Rod due to Impact Load
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Verified Stress Induced in Rod due to Impact Load
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Verified Stress Induced in Rod due to Impact Load if Height through which Load Dropped is Zero
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Verified Value of Load Applied with Impact given Work Done by Load
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Verified Value of Load Dropped if Height through which Load Dropped is Zero
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Verified Work Done by Load for Small Extension of Rod
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Stress (4)
Created Area of Body given Stress
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Created Change in Length given Longitudinal Stress
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Created Normal Stress or Longitudinal Stress
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Created Original Length given Longitudinal Stress
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1 More Stress Calculators
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Verified Distance between Neutral and Considered Layer in Beam
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Verified Distance between Neutral and Considered Layer using Moment of Resistance
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Verified Distance between Neutral and Considered Layers in Beams
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Verified Force on Layer at Distance from Neutral Layer of Beam
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Verified Force on Layer of Beams given Stress in Layer
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Verified Moment of Inertia of Area of Section given Young's Modulus of Beam
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Verified Moment of Inertia of Area of Section of Beam given Stress in Layer
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Verified Moment of Resistance
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Verified Moment of Resistance using Stress in Layer of Beam
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Verified Radius of Neutral Axis using Moment of Resistance
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Verified Radius of Neutral Layer
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Verified Radius of Neutral Layer given Force on Considered Layer
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Verified Stress in Layer Considering that Beam is Subjected to Simple Bending
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Verified Stress in Layer of Beam given Force on Layer
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Verified Stress in Layer of Beam given Moment of Resistance
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Verified Young's Modulus of Beam
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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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Created Sum of 4th Powers of First N Natural Numbers
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6 More Sum of 4th Powers Calculators
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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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Verified Sum of Total Terms of Arithmetic Progression given Last Term
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7 More Sum of Terms of Arithmetic Progression Calculators
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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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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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Verified Circular Frequency due to Uniformly Distributed Load
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Verified Circular Frequency given Static Deflection
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Verified Length of Shaft given Circular Frequency
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Verified Length of Shaft given Natural Frequency
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Verified Length of Shaft given Static Deflection
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Verified Maximum Bending Moment at Distance x from End A
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Verified Moment of Inertia of Shaft given Circular Frequency
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Verified Moment of Inertia of Shaft given Natural Frequency
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Verified Moment of Inertia of Shaft given Static Deflection given Load per Unit Length
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Verified Natural Frequency due to Uniformly Distributed Load
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Verified Natural Frequency given Static Deflection
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Verified Static Deflection at Distance x from End A
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Verified Static Deflection of Simply Supported Shaft due to Uniformly Distributed Load
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Verified Static Deflection using Natural Frequency
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Verified Uniformly Distributed Load Unit Length given Circular Frequency
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Verified Uniformly Distributed Load Unit Length given Natural Frequency
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Verified Uniformly Distributed Load Unit Length given Static Deflection
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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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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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Verified 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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Created Distance from Start given Restoring Force and Constant K
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Created Distance Traveled by Particle in SHM until Velocity becomes Zero
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Created Distance Traveled given Velocity
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Created Distance Traveled in SHM given Angular Frequency
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Created Square of Different Distances Traveled in SHM
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Created Total Distance Traveled given Velocity and Angular Frequency
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Created Velocity of Particle in SHM
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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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