Torsional shear stress in side-crankshaft below flywheel for max torque Calculator

✖Diameter of Shaft Under Flywheel is the diameter, of the part of the crankshaft under the flywheel, the distance across the shaft that passes through the center of the shaft is 2R (twice the radius).ⓘ Diameter of Shaft Under Flywheel [D_s]			+10% -10%
✖Vertical Bending Moment in Shaft Under Flywheel is the bending moment in the vertical plane of the part of crankshaft under the flywheel.ⓘ Vertical Bending Moment in Shaft Under Flywheel [M_bv]			+10% -10%
✖Horizontal Bending Moment in Shaft under Flywheel is the bending moment in the horizontal plane of the part of the crankshaft under the flywheel.ⓘ Horizontal Bending Moment in Shaft Under Flywheel [M_bh]			+10% -10%
✖Tangential Force at Crank Pin is the component of thrust force on connecting rod acting at the crankpin in the direction tangential to the connecting rod.ⓘ Tangential Force at Crank Pin [P_t]			+10% -10%
✖Distance Between Crank Pin And Crankshaft is the perpendicular distance between the crank pin and the crankshaft.ⓘ Distance Between Crank Pin And Crankshaft [r]			+10% -10%

✖Shear Stress in Crankshaft Under Flywheel is the amount of shear stress (causes deformation by slippage along plane parallel to the imposed stress) at the crankshaft part under flywheel.ⓘ Torsional shear stress in side-crankshaft below flywheel for max torque [τ]

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Torsional shear stress in side-crankshaft below flywheel for max torque Solution

STEP 0: Pre-Calculation Summary

Formula Used

Shear Stress in Crankshaft Under Flywheel = 16/(pi*Diameter of Shaft Under Flywheel^3)*sqrt(Vertical Bending Moment in Shaft Under Flywheel^2+Horizontal Bending Moment in Shaft Under Flywheel^2+(Tangential Force at Crank Pin*Distance Between Crank Pin And Crankshaft)^2)
τ = 16/(pi*D_s^3)*sqrt(M_bv^2+M_bh^2+(P_t*r)^2)
This formula uses 1 Constants, 1 Functions, 6 Variables

Constants Used

pi - Archimedes' constant Value Taken As 3.14159265358979323846264338327950288

Functions Used

sqrt - A square root function is a function that takes a non-negative number as an input and returns the square root of the given input number., sqrt(Number)

Variables Used

Shear Stress in Crankshaft Under Flywheel - (Measured in Pascal) - Shear Stress in Crankshaft Under Flywheel is the amount of shear stress (causes deformation by slippage along plane parallel to the imposed stress) at the crankshaft part under flywheel.
Diameter of Shaft Under Flywheel - (Measured in Meter) - Diameter of Shaft Under Flywheel is the diameter, of the part of the crankshaft under the flywheel, the distance across the shaft that passes through the center of the shaft is 2R (twice the radius).
Vertical Bending Moment in Shaft Under Flywheel - (Measured in Newton Meter) - Vertical Bending Moment in Shaft Under Flywheel is the bending moment in the vertical plane of the part of crankshaft under the flywheel.
Horizontal Bending Moment in Shaft Under Flywheel - (Measured in Newton Meter) - Horizontal Bending Moment in Shaft under Flywheel is the bending moment in the horizontal plane of the part of the crankshaft under the flywheel.
Tangential Force at Crank Pin - (Measured in Newton) - Tangential Force at Crank Pin is the component of thrust force on connecting rod acting at the crankpin in the direction tangential to the connecting rod.
Distance Between Crank Pin And Crankshaft - (Measured in Meter) - Distance Between Crank Pin And Crankshaft is the perpendicular distance between the crank pin and the crankshaft.

STEP 1: Convert Input(s) to Base Unit

Diameter of Shaft Under Flywheel: 35.43213 Millimeter --> 0.03543213 Meter (Check conversion here)
Vertical Bending Moment in Shaft Under Flywheel: 25000 Newton Millimeter --> 25 Newton Meter (Check conversion here)
Horizontal Bending Moment in Shaft Under Flywheel: 82400 Newton Millimeter --> 82.4 Newton Meter (Check conversion here)
Tangential Force at Crank Pin: 3613.665 Newton --> 3613.665 Newton No Conversion Required
Distance Between Crank Pin And Crankshaft: 10.5 Millimeter --> 0.0105 Meter (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

τ = 16/(pi*D_s^3)*sqrt(M_bv^2+M_bh^2+(P_t*r)^2) --> 16/(pi*0.03543213^3)*sqrt(25^2+82.4^2+(3613.665*0.0105)^2)

Evaluating ... ...

τ = 10773568.0928511

STEP 3: Convert Result to Output's Unit

10773568.0928511 Pascal -->10.7735680928511 Newton per Square Millimeter (Check conversion here)

FINAL ANSWER

10.7735680928511 ≈ 10.77357 Newton per Square Millimeter <-- Shear Stress in Crankshaft Under Flywheel

(Calculation completed in 00.020 seconds)

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Home » Physics » IC Engine » Design of IC Engine Components » Crankshaft » Design of Side Crankshaft » Mechanical » Design of Shaft Under Flywheel at Angle of Maximum Torque » Torsional shear stress in side-crankshaft below flywheel for max torque

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< Design of Shaft Under Flywheel at Angle of Maximum Torque Calculators

Horizontal Bending Moment at Central Plane of Side Crankshaft below Flywheel at max Torque

LaTeX Go Horizontal Bending Moment in Shaft Under Flywheel = (Tangential Force at Crank Pin*(Overhang Distance of Piston Force From Bearing1+Side Crankshaft Bearing1 Gap From Flywheel))-(Side Crankshaft Bearing1 Gap From Flywheel*(Horizontal Force at Bearing1 By Tangential Force+Horizontal Reaction at Bearing 1 Due to Belt))

Vertical bending moment at central plane of side crankshaft below flywheel at max torque

LaTeX Go Vertical Bending Moment in Shaft Under Flywheel = (Radial Force at Crank Pin*(Overhang Distance of Piston Force From Bearing1+Side Crankshaft Bearing1 Gap From Flywheel))-(Side Crankshaft Bearing1 Gap From Flywheel*(Vertical Reaction at Bearing 1 Due to Radial Force+Vertical Reaction at Bearing 1 Due to Flywheel))

Torsional shear stress in side-crankshaft below flywheel for max torque

LaTeX Go Shear Stress in Crankshaft Under Flywheel = 16/(pi*Diameter of Shaft Under Flywheel^3)*sqrt(Vertical Bending Moment in Shaft Under Flywheel^2+Horizontal Bending Moment in Shaft Under Flywheel^2+(Tangential Force at Crank Pin*Distance Between Crank Pin And Crankshaft)^2)

Resultant Bending moment at side crankshaft below flywheel at max torque given moments

LaTeX Go Total Bending Moment in Crankshaft Under Flywheel = sqrt(Vertical Bending Moment in Shaft Under Flywheel^2+Horizontal Bending Moment in Shaft Under Flywheel^2)

Torsional shear stress in side-crankshaft below flywheel for max torque Formula

LaTeX Go

What is an Engine?

An engine is a machine designed to convert one or more forms of energy into mechanical energy. Mechanical heat engines convert heat into work via various thermodynamic processes. Engines – such as the ones used to run vehicles – can run on a variety of different fuels, most notably gasoline and diesel in the case of cars. The internal combustion engine is perhaps the most common example of a chemical heat engine, in which heat from the combustion of fuel causes rapid pressurization of the gaseous combustion products in the combustion chamber, causing them to expand and drive a piston, which turns a crankshaft.

How to Calculate Torsional shear stress in side-crankshaft below flywheel for max torque?

Torsional shear stress in side-crankshaft below flywheel for max torque calculator uses Shear Stress in Crankshaft Under Flywheel = 16/(pi*Diameter of Shaft Under Flywheel^3)*sqrt(Vertical Bending Moment in Shaft Under Flywheel^2+Horizontal Bending Moment in Shaft Under Flywheel^2+(Tangential Force at Crank Pin*Distance Between Crank Pin And Crankshaft)^2) to calculate the Shear Stress in Crankshaft Under Flywheel, The torsional shear stress in side-crankshaft below flywheel for max torque is the torsional shear stress induced in the crankshaft portion under the flywheel, as a result of the torsional moment onto the crankshaft, when the side crankshaft is designed for the maximum torsional moment. Shear Stress in Crankshaft Under Flywheel is denoted by τ symbol.

How to calculate Torsional shear stress in side-crankshaft below flywheel for max torque using this online calculator? To use this online calculator for Torsional shear stress in side-crankshaft below flywheel for max torque, enter Diameter of Shaft Under Flywheel (D_s), Vertical Bending Moment in Shaft Under Flywheel (M_bv), Horizontal Bending Moment in Shaft Under Flywheel (M_bh), Tangential Force at Crank Pin (P_t) & Distance Between Crank Pin And Crankshaft (r) and hit the calculate button. Here is how the Torsional shear stress in side-crankshaft below flywheel for max torque calculation can be explained with given input values -> 1.4E-5 = 16/(pi*0.03543213^3)*sqrt(25^2+82.4^2+(3613.665*0.0105)^2).

FAQ

What is Torsional shear stress in side-crankshaft below flywheel for max torque?

The torsional shear stress in side-crankshaft below flywheel for max torque is the torsional shear stress induced in the crankshaft portion under the flywheel, as a result of the torsional moment onto the crankshaft, when the side crankshaft is designed for the maximum torsional moment and is represented as τ = 16/(pi*D_s^3)*sqrt(M_bv^2+M_bh^2+(P_t*r)^2) or Shear Stress in Crankshaft Under Flywheel = 16/(pi*Diameter of Shaft Under Flywheel^3)*sqrt(Vertical Bending Moment in Shaft Under Flywheel^2+Horizontal Bending Moment in Shaft Under Flywheel^2+(Tangential Force at Crank Pin*Distance Between Crank Pin And Crankshaft)^2). Diameter of Shaft Under Flywheel is the diameter, of the part of the crankshaft under the flywheel, the distance across the shaft that passes through the center of the shaft is 2R (twice the radius), Vertical Bending Moment in Shaft Under Flywheel is the bending moment in the vertical plane of the part of crankshaft under the flywheel, Horizontal Bending Moment in Shaft under Flywheel is the bending moment in the horizontal plane of the part of the crankshaft under the flywheel, Tangential Force at Crank Pin is the component of thrust force on connecting rod acting at the crankpin in the direction tangential to the connecting rod & Distance Between Crank Pin And Crankshaft is the perpendicular distance between the crank pin and the crankshaft.

How to calculate Torsional shear stress in side-crankshaft below flywheel for max torque?

The torsional shear stress in side-crankshaft below flywheel for max torque is the torsional shear stress induced in the crankshaft portion under the flywheel, as a result of the torsional moment onto the crankshaft, when the side crankshaft is designed for the maximum torsional moment is calculated using Shear Stress in Crankshaft Under Flywheel = 16/(pi*Diameter of Shaft Under Flywheel^3)*sqrt(Vertical Bending Moment in Shaft Under Flywheel^2+Horizontal Bending Moment in Shaft Under Flywheel^2+(Tangential Force at Crank Pin*Distance Between Crank Pin And Crankshaft)^2). To calculate Torsional shear stress in side-crankshaft below flywheel for max torque, you need Diameter of Shaft Under Flywheel (D_s), Vertical Bending Moment in Shaft Under Flywheel (M_bv), Horizontal Bending Moment in Shaft Under Flywheel (M_bh), Tangential Force at Crank Pin (P_t) & Distance Between Crank Pin And Crankshaft (r). With our tool, you need to enter the respective value for Diameter of Shaft Under Flywheel, Vertical Bending Moment in Shaft Under Flywheel, Horizontal Bending Moment in Shaft Under Flywheel, Tangential Force at Crank Pin & Distance Between Crank Pin And Crankshaft 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 Shear Stress in Crankshaft Under Flywheel?

In this formula, Shear Stress in Crankshaft Under Flywheel uses Diameter of Shaft Under Flywheel, Vertical Bending Moment in Shaft Under Flywheel, Horizontal Bending Moment in Shaft Under Flywheel, Tangential Force at Crank Pin & Distance Between Crank Pin And Crankshaft. We can use 1 other way(s) to calculate the same, which is/are as follows -

Shear Stress in Crankshaft Under Flywheel = 16/(pi*Diameter of Shaft Under Flywheel^3)*sqrt(Total Bending Moment in Crankshaft Under Flywheel^2+Torsional Moment at Crankshaft Under Flywheel^2)

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