Resolved shear stress Solution

STEP 0: Pre-Calculation Summary
Formula Used
Resolved shear stress = Applied Stress*cos(Slip plane angle)*cos(Slip direction angle)
𝛕R = σ*cos(ϕ)*cos(λ)
This formula uses 1 Functions, 4 Variables
Functions Used
cos - Cosine of an angle is the ratio of the side adjacent to the angle to the hypotenuse of the triangle., cos(Angle)
Variables Used
Resolved shear stress - (Measured in Pascal) - Resolved shear stress is the shear component that exists at all but parallel or perpendicular alignments to the stress direction.
Applied Stress - (Measured in Pascal) - Applied stress is denoted by the symbol σ.
Slip plane angle - (Measured in Radian) - Slip plane angle is the angle between the normal to the slip plane and the applied stress direction.
Slip direction angle - (Measured in Radian) - Slip direction angle is the angle between the slip and stress directions.
STEP 1: Convert Input(s) to Base Unit
Applied Stress: 93.3 Pascal --> 93.3 Pascal No Conversion Required
Slip plane angle: 30 Degree --> 0.5235987755982 Radian (Check conversion ​here)
Slip direction angle: 30 Degree --> 0.5235987755982 Radian (Check conversion ​here)
STEP 2: Evaluate Formula
Substituting Input Values in Formula
𝛕R = σ*cos(ϕ)*cos(λ) --> 93.3*cos(0.5235987755982)*cos(0.5235987755982)
Evaluating ... ...
𝛕R = 69.975
STEP 3: Convert Result to Output's Unit
69.975 Pascal -->6.9975E-05 Megapascal (Check conversion ​here)
FINAL ANSWER
6.9975E-05 7E-5 Megapascal <-- Resolved shear stress
(Calculation completed in 00.004 seconds)

Credits

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Created by Hariharan V S
Indian Institute of Technology (IIT), Chennai
Hariharan V S has created this Calculator and 25+ more calculators!
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Resolved shear stress Formula

​LaTeX ​Go
Resolved shear stress = Applied Stress*cos(Slip plane angle)*cos(Slip direction angle)
𝛕R = σ*cos(ϕ)*cos(λ)

Resolved Shear Stress

Even though an applied stress may be pure tensile (or compressive), shear components exist at all but parallel or perpendicular alignments to the stress direction.These are termed resolved shear stresses, and their magnitudes depend not only on the applied stress, but also on the orientation of both the slip plane and direction within that plane.

How to Calculate Resolved shear stress?

Resolved shear stress calculator uses Resolved shear stress = Applied Stress*cos(Slip plane angle)*cos(Slip direction angle) to calculate the Resolved shear stress, Resolved shear stress is the shear component that exists at all but parallel or perpendicular alignments to the stress direction. Resolved shear stress is denoted by 𝛕R symbol.

How to calculate Resolved shear stress using this online calculator? To use this online calculator for Resolved shear stress, enter Applied Stress (σ), Slip plane angle (ϕ) & Slip direction angle (λ) and hit the calculate button. Here is how the Resolved shear stress calculation can be explained with given input values -> 7E-11 = 93.3*cos(0.5235987755982)*cos(0.5235987755982).

FAQ

What is Resolved shear stress?
Resolved shear stress is the shear component that exists at all but parallel or perpendicular alignments to the stress direction and is represented as 𝛕R = σ*cos(ϕ)*cos(λ) or Resolved shear stress = Applied Stress*cos(Slip plane angle)*cos(Slip direction angle). Applied stress is denoted by the symbol σ, Slip plane angle is the angle between the normal to the slip plane and the applied stress direction & Slip direction angle is the angle between the slip and stress directions.
How to calculate Resolved shear stress?
Resolved shear stress is the shear component that exists at all but parallel or perpendicular alignments to the stress direction is calculated using Resolved shear stress = Applied Stress*cos(Slip plane angle)*cos(Slip direction angle). To calculate Resolved shear stress, you need Applied Stress (σ), Slip plane angle (ϕ) & Slip direction angle (λ). With our tool, you need to enter the respective value for Applied Stress, Slip plane angle & Slip direction angle and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.
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