Work Done for Punching a Hole Calculator

Category	Physics ↺
Physics	Theory of Machine ↺
Theory-Of-Machine	Turning Moment Diagrams and Flywheel ↺

✖Shear Force is the force which causes shear deformation to occur in the shear plane.ⓘ Shear Force [Fs]			+10% -10%
✖Thickness of the material to be punched is the measure of the smallest dimension of the material.ⓘ Thickness of the material to be punched [t]			+10% -10%

✖Work is done when a force that is applied to an object moves that object.ⓘ Work Done for Punching a Hole [W]

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Saiju Shah

Jayawant Shikshan Prasarak Mandal (JSPM), Pune

Saiju Shah has created this Calculator and 500+ more calculators!

Himanshi Sharma

Bhilai Institute of Technology (BIT), Raipur

Himanshi Sharma has verified this Calculator and 500+ more calculators!

< 11 Other formulas that you can solve using the same Inputs

Distance of C.G of the area(above considered level) from neutral axis

Distance of the C.G of the area from N.A=(Shear Stress*M.I of the area of section*Width of beam at considered level )/(Shear Force*Area of the section above considered level) Go

Moment of the inertia of section about neutral axis

M.I of the area of section=(Shear Force*Area of the section above considered level*Distance of the C.G of the area from N.A)/(Shear Stress*Width of beam at considered level ) Go

Area of the section above considered level

Area of the section above considered level=(Shear Stress*M.I of the area of section*Width of beam at considered level )/(Shear Force*Distance of the C.G of the area from N.A) Go

Width of the beam at considered level

Width of beam at considered level =(Shear Force*Area of the section above considered level*Distance of the C.G of the area from N.A)/(M.I of the area of section*Shear Stress) Go

Shear stress at the section

Shear Stress=(Shear Force*Area of the section above considered level*Distance of the C.G of the area from N.A)/(M.I of the area of section*Width of beam at considered level ) Go

Cutting force for given force along the shear force, thrust force, and shear angle

Cutting Force=(Shear Force+(Axial Thrust*(sin(Shear Angle))))/(cos(Shear Angle)) Go

Thrust force for given cutting force, shear angle & force along the shear force

Axial Thrust=((Cutting Force*(cos(Shear Angle)))-Shear Force)/(sin(Shear Angle)) Go

Shear Modulus of Elasticity when Strain Energy in Shear is Given

Shear Modulus of Elasticity=(Shear Force^2)*Length/(2*Shear Area*Strain Energy) Go

Shear Area when Strain Energy in Shear is Given

Shear Area=(Shear Force^2)*Length/(2*Strain Energy*Shear Modulus of Elasticity) Go

Strain Energy in Shear

Strain Energy=(Shear Force^2)*Length/(2*Shear Area*Shear Modulus of Elasticity) Go

Length over which Deformation Takes Place when Strain Energy in Shear is Given

Length=2*Strain Energy*Shear Area*Shear Modulus of Elasticity/(Shear Force^2) Go

< 11 Other formulas that calculate the same Output

Work done in adiabatic process

Work =(Initial Pressure of System*Initial Volume of System-Final Pressure of System*Final Volume of System)/(Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume-1) Go

Expansion Work

Work =Mass of air*Specific Heat Capacity at Constant Pressure*(Temperature at the end of cooling process-Actual temperature at end of isentropic expansion) Go

Compression Work

Work =Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Actual temperature of Rammed Air) Go

Work done in one revolution for belt transmission dynamometer

Work =(Tensions in the tight side of belt-Tensions in the slack side of belt)*pi*Diameter of the driving pulley Go

Work done per revolution for rope brake dynamometer

Work =(Dead load-Spring balance reading)*pi*(Diameter of the wheel+diameter of rope) Go

Work done in isothermal process (using pressure)

Work =[R]*Temperature of Gas*ln(Initial Pressure of System/Final Pressure of System) Go

Work done in isothermal process (using volume)

Work =[R]*Temperature of Gas*ln(Final Volume of System/Initial Volume of System) Go

Work done in adiabatic process

Work =(Mass of Gas*[R]*(initial temp.-final temp.))/(Heat Capacity Ratio-1) Go

Work done in an isobaric process

Work =Number of Moles*[R]*Temperature Difference Go

Work

Work =Force*Displacement*cos(Angle A) Go

Work done in one revolution for prony brake dynamometer

Work =Torque*2*pi Go

Work Done for Punching a Hole Formula

Work =Shear Force*Thickness of the material to be punched
W=Fs*t

More formulas

Accelerating torque on the rotating parts of the engine Go

Coefficient of Fluctuation of Energy Go

Mean linear velocity Go

Mean angular speed Go

Mean speed in r.p.m Go

Coefficient of Fluctuation of Speed for flywheel Go

Coefficient of steadiness Go

Maximum Fluctuation of Energy Go

Hoop Stress in Flywheel Go

Centrifugal Stress Go

Maximum shear force required for punching Go

Stroke of the Punch Go

What causes shear force?

Shearing forces are unaligned forces pushing one part of a body in one direction, and another part of the body in the opposite direction. A shear force is a force applied perpendicular to a surface, in opposition to an offset force acting in the opposite direction. This results in a shear strain. In simple terms, one part of the surface is pushed in one direction, while another part of the surface is pushed in the opposite direction.

How to Calculate Work Done for Punching a Hole?

Work Done for Punching a Hole calculator uses Work =Shear Force*Thickness of the material to be punched to calculate the Work , Work Done for Punching a Hole is the total amount of work to punch a hole which purely depends upon the amount of force (F) causing the work. Work and is denoted by W symbol.

How to calculate Work Done for Punching a Hole using this online calculator? To use this online calculator for Work Done for Punching a Hole, enter Shear Force (Fs) and Thickness of the material to be punched (t) and hit the calculate button. Here is how the Work Done for Punching a Hole calculation can be explained with given input values -> 0.5 = 50*0.01.

FAQ

What is Work Done for Punching a Hole?

Work Done for Punching a Hole is the total amount of work to punch a hole which purely depends upon the amount of force (F) causing the work and is represented as W=Fs*t or Work =Shear Force*Thickness of the material to be punched. Shear Force is the force which causes shear deformation to occur in the shear plane and Thickness of the material to be punched is the measure of the smallest dimension of the material.

How to calculate Work Done for Punching a Hole?

Work Done for Punching a Hole is the total amount of work to punch a hole which purely depends upon the amount of force (F) causing the work is calculated using Work =Shear Force*Thickness of the material to be punched. To calculate Work Done for Punching a Hole, you need Shear Force (Fs) and Thickness of the material to be punched (t). With our tool, you need to enter the respective value for Shear Force and Thickness of the material to be punched and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Work ?

In this formula, Work uses Shear Force and Thickness of the material to be punched. We can use 11 other way(s) to calculate the same, which is/are as follows -

Work =Force*Displacement*cos(Angle A)
Work =Number of Moles*[R]*Temperature Difference
Work =[R]*Temperature of Gas*ln(Initial Pressure of System/Final Pressure of System)
Work =[R]*Temperature of Gas*ln(Final Volume of System/Initial Volume of System)
Work =(Initial Pressure of System*Initial Volume of System-Final Pressure of System*Final Volume of System)/(Molar Specific Heat Capacity at Constant Pressure/Molar Specific Heat Capacity at Constant Volume-1)
Work =(Mass of Gas*[R]*(initial temp.-final temp.))/(Heat Capacity Ratio-1)
Work =Torque*2*pi
Work =(Dead load-Spring balance reading)*pi*(Diameter of the wheel+diameter of rope)
Work =(Tensions in the tight side of belt-Tensions in the slack side of belt)*pi*Diameter of the driving pulley
Work =Mass of air*Specific Heat Capacity at Constant Pressure*(Actual end temp of isentropic compression-Actual temperature of Rammed Air)
Work =Mass of air*Specific Heat Capacity at Constant Pressure*(Temperature at the end of cooling process-Actual temperature at end of isentropic expansion)

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