Maximum compressive stress in crankweb of side crankshaft for max torque Calculator

✖Compressive stress in crank web central plane is the magnitude of force applied onto the crank web, divided by cross-sectional area of crank web in a direction perpendicular to the applied force.ⓘ Compressive Stress in Crank Web Central Plane [σ_c]			+10% -10%
✖Shear Stress in Crankweb is the amount of shear stress (causes deformation by slippage along plane parallel to the imposed stress) in the crankweb.ⓘ Shear Stress in Crankweb [τ]			+10% -10%

✖Maximum Compressive Stress in Crank Web is stress in Crank Web as a result of compressive stress by radial thrust on connecting rod, & bending stress by tangential & radial components of thrust force.ⓘ Maximum compressive stress in crankweb of side crankshaft for max torque [σ_max]

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Maximum compressive stress in crankweb of side crankshaft for max torque Solution

STEP 0: Pre-Calculation Summary

Formula Used

Maximum Compressive Stress in Crank Web = Compressive Stress in Crank Web Central Plane/2+(sqrt(Compressive Stress in Crank Web Central Plane^2+(4*Shear Stress in Crankweb^2)))/2
σ_max = σ_c/2+(sqrt(σ_c^2+(4*τ^2)))/2
This formula uses 1 Functions, 3 Variables

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

Maximum Compressive Stress in Crank Web - (Measured in Pascal) - Maximum Compressive Stress in Crank Web is stress in Crank Web as a result of compressive stress by radial thrust on connecting rod, & bending stress by tangential & radial components of thrust force.
Compressive Stress in Crank Web Central Plane - (Measured in Pascal) - Compressive stress in crank web central plane is the magnitude of force applied onto the crank web, divided by cross-sectional area of crank web in a direction perpendicular to the applied force.
Shear Stress in Crankweb - (Measured in Pascal) - Shear Stress in Crankweb is the amount of shear stress (causes deformation by slippage along plane parallel to the imposed stress) in the crankweb.

STEP 1: Convert Input(s) to Base Unit

Compressive Stress in Crank Web Central Plane: 16.61 Newton per Square Millimeter --> 16610000 Pascal (Check conversion here)
Shear Stress in Crankweb: 10 Newton per Square Millimeter --> 10000000 Pascal (Check conversion here)

STEP 2: Evaluate Formula

Substituting Input Values in Formula

σ_max = σ_c/2+(sqrt(σ_c^2+(4*τ^2)))/2 --> 16610000/2+(sqrt(16610000^2+(4*10000000^2)))/2

Evaluating ... ...

σ_max = 21303962.4585965

STEP 3: Convert Result to Output's Unit

21303962.4585965 Pascal -->21.3039624585965 Newton per Square Millimeter (Check conversion here)

FINAL ANSWER

21.3039624585965 ≈ 21.30396 Newton per Square Millimeter <-- Maximum Compressive Stress in Crank Web

(Calculation completed in 00.004 seconds)

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Home » Physics » IC Engine » Design of IC Engine Components » Crankshaft » Design of Side Crankshaft » Mechanical » Design of Crank Web at Angle of Maximum Torque » Maximum compressive stress in crankweb of side crankshaft for max torque

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< Design of Crank Web at Angle of Maximum Torque Calculators

Bending stress in crankweb of side crankshaft due to radial thrust for max torque

LaTeX Go Bending Stress in Crankweb Due to Radial Force = (6*Radial Force at Crank Pin*((Length of Crank Pin*0.75)+(Thickness of Crank Web*0.5)))/(Thickness of Crank Web^2*Width of Crank Web)

Bending stress in crankweb of side crankshaft due to radial thrust for max torque given moment

LaTeX Go Bending Stress in Crankweb Due to Radial Force = (6*Bending Moment in Crankweb Due to Radial Force)/(Thickness of Crank Web^2*Width of Crank Web)

Bending moment in crankweb of side crankshaft due to radial thrust for max torque given stress

LaTeX Go Bending Moment in Crankweb Due to Radial Force = (Bending Stress in Crankweb Due to Radial Force*Thickness of Crank Web^2*Width of Crank Web)/6

Bending moment in crankweb of side crankshaft due to radial thrust for maximum torque

LaTeX Go Bending Moment in Crankweb Due to Radial Force = Radial Force at Crank Pin*((Length of Crank Pin*0.75)+(Thickness of Crank Web*0.5))

Maximum compressive stress in crankweb of side crankshaft for max torque Formula

LaTeX Go

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How to Calculate Maximum compressive stress in crankweb of side crankshaft for max torque?

Maximum compressive stress in crankweb of side crankshaft for max torque calculator uses Maximum Compressive Stress in Crank Web = Compressive Stress in Crank Web Central Plane/2+(sqrt(Compressive Stress in Crank Web Central Plane^2+(4*Shear Stress in Crankweb^2)))/2 to calculate the Maximum Compressive Stress in Crank Web, Maximum compressive stress in crankweb of side crankshaft for max torque is the maximum compressive stress induced into the crank web as a result of the direct compressive stress due to radial thrust on connecting rod, and bending stress due to the tangential and radial components of thrust force and when the side crankshaft is designed for maximum torsional moment. Maximum Compressive Stress in Crank Web is denoted by σ_max symbol.

How to calculate Maximum compressive stress in crankweb of side crankshaft for max torque using this online calculator? To use this online calculator for Maximum compressive stress in crankweb of side crankshaft for max torque, enter Compressive Stress in Crank Web Central Plane (σ_c) & Shear Stress in Crankweb (τ) and hit the calculate button. Here is how the Maximum compressive stress in crankweb of side crankshaft for max torque calculation can be explained with given input values -> 2.4E-5 = 16610000/2+(sqrt(16610000^2+(4*10000000^2)))/2.

FAQ

What is Maximum compressive stress in crankweb of side crankshaft for max torque?

Maximum compressive stress in crankweb of side crankshaft for max torque is the maximum compressive stress induced into the crank web as a result of the direct compressive stress due to radial thrust on connecting rod, and bending stress due to the tangential and radial components of thrust force and when the side crankshaft is designed for maximum torsional moment and is represented as σ_max = σ_c/2+(sqrt(σ_c^2+(4*τ^2)))/2 or Maximum Compressive Stress in Crank Web = Compressive Stress in Crank Web Central Plane/2+(sqrt(Compressive Stress in Crank Web Central Plane^2+(4*Shear Stress in Crankweb^2)))/2. Compressive stress in crank web central plane is the magnitude of force applied onto the crank web, divided by cross-sectional area of crank web in a direction perpendicular to the applied force & Shear Stress in Crankweb is the amount of shear stress (causes deformation by slippage along plane parallel to the imposed stress) in the crankweb.

How to calculate Maximum compressive stress in crankweb of side crankshaft for max torque?

Maximum compressive stress in crankweb of side crankshaft for max torque is the maximum compressive stress induced into the crank web as a result of the direct compressive stress due to radial thrust on connecting rod, and bending stress due to the tangential and radial components of thrust force and when the side crankshaft is designed for maximum torsional moment is calculated using Maximum Compressive Stress in Crank Web = Compressive Stress in Crank Web Central Plane/2+(sqrt(Compressive Stress in Crank Web Central Plane^2+(4*Shear Stress in Crankweb^2)))/2. To calculate Maximum compressive stress in crankweb of side crankshaft for max torque, you need Compressive Stress in Crank Web Central Plane (σ_c) & Shear Stress in Crankweb (τ). With our tool, you need to enter the respective value for Compressive Stress in Crank Web Central Plane & Shear Stress in Crankweb 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 Maximum Compressive Stress in Crank Web?

In this formula, Maximum Compressive Stress in Crank Web uses Compressive Stress in Crank Web Central Plane & Shear Stress in Crankweb. We can use 1 other way(s) to calculate the same, which is/are as follows -

Maximum Compressive Stress in Crank Web = (Direct Compressive Stress in Crankweb+Bending Stress in Crankweb Due to Radial Force+Bending Stress in Crankweb Due to Tangential Force)/2+(sqrt((Direct Compressive Stress in Crankweb+Bending Stress in Crankweb Due to Radial Force+Bending Stress in Crankweb Due to Tangential Force)^2+(4*Shear Stress in Crankweb^2)))/2

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