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Shear Stress When Member Subjected To Axial Load Calculator

Formula Used:

\[ \tau_{\theta} = 0.5 \times \sigma_y \times \sin(2\theta) \]

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rad

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1. What is Shear Stress on Oblique Plane?

Shear stress on an oblique plane refers to the component of stress that acts parallel to the plane when a member is subjected to axial loading. It is an important parameter in material strength analysis and failure prediction.

2. How Does the Calculator Work?

The calculator uses the formula:

\[ \tau_{\theta} = 0.5 \times \sigma_y \times \sin(2\theta) \]

Where:

Explanation: This formula calculates the shear stress component on a plane oriented at angle θ to the direction of applied stress.

3. Importance of Shear Stress Calculation

Details: Calculating shear stress on oblique planes is crucial for understanding material behavior under complex loading conditions, predicting failure modes, and designing structural components that can withstand combined stress states.

4. Using the Calculator

Tips: Enter stress value in Pascals (Pa) and angle in radians. Ensure all values are positive and angle is within valid range (0 to π/2 radians for physical significance).

5. Frequently Asked Questions (FAQ)

Q1: What is the physical significance of shear stress on oblique planes?
A: It helps determine the maximum shear stress in a material and identifies potential failure planes where material yielding might initiate.

Q2: How does the angle θ affect the shear stress?
A: Shear stress reaches its maximum value when θ = 45° (π/4 radians) and becomes zero when θ = 0° or 90°.

Q3: Can this formula be used for any material?
A: Yes, this is a general formula derived from stress transformation equations and applies to isotropic materials under uniaxial loading.

Q4: What are the units for the input parameters?
A: Stress should be in Pascals (Pa) and angle should be in radians. 1 MPa = 1,000,000 Pa.

Q5: How is this different from normal stress on oblique planes?
A: Normal stress acts perpendicular to the plane, while shear stress acts parallel to the plane. Both are components of the total stress acting on the oblique plane.

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