Math Problem Statement

A plane stress element has σx= 80 MPa,σy = 20 MPa, and τxy= 50 MPa cw (a)Using Mohr’s circle, find the principal stresses, maximum shear stress and direction.

Solution

To solve this problem using Mohr's Circle, we'll follow these steps:

Given Data:

  • σx=80\sigma_x = 80 MPa (stress in the x-direction)
  • σy=20\sigma_y = 20 MPa (stress in the y-direction)
  • τxy=50\tau_{xy} = 50 MPa (shear stress, clockwise)

Step 1: Determine the Center and Radius of Mohr's Circle

The center CC of Mohr's circle is located at: C=(σx+σy2,0)C = \left(\frac{\sigma_x + \sigma_y}{2}, 0\right) C=(80+202,0)=(50,0) MPaC = \left(\frac{80 + 20}{2}, 0\right) = (50, 0) \text{ MPa}

The radius RR of Mohr's circle is given by: R=(σxσy2)2+τxy2R = \sqrt{\left(\frac{\sigma_x - \sigma_y}{2}\right)^2 + \tau_{xy}^2} R=(80202)2+502=302+502=900+2500=340058.31 MPaR = \sqrt{\left(\frac{80 - 20}{2}\right)^2 + 50^2} = \sqrt{30^2 + 50^2} = \sqrt{900 + 2500} = \sqrt{3400} \approx 58.31 \text{ MPa}

Step 2: Principal Stresses

The principal stresses σ1\sigma_1 and σ2\sigma_2 are located at the points on Mohr's circle along the horizontal axis. They are calculated as: σ1=C+R=50+58.31=108.31 MPa\sigma_1 = C + R = 50 + 58.31 = 108.31 \text{ MPa} σ2=CR=5058.31=8.31 MPa\sigma_2 = C - R = 50 - 58.31 = -8.31 \text{ MPa}

Step 3: Maximum Shear Stress

The maximum shear stress τmax\tau_{\text{max}} occurs at the top (or bottom) of Mohr's circle, which is equal to the radius: τmax=R=58.31 MPa\tau_{\text{max}} = R = 58.31 \text{ MPa}

The corresponding normal stress at the maximum shear stress is the center CC of Mohr's circle: σavg=C=50 MPa\sigma_{\text{avg}} = C = 50 \text{ MPa}

Step 4: Direction of Principal Stresses and Maximum Shear Stress

To find the angle θp\theta_p that the principal stresses make with the x-axis (in the physical space), use: tan(2θp)=2τxyσxσy\tan(2\theta_p) = \frac{2\tau_{xy}}{\sigma_x - \sigma_y} tan(2θp)=2×508020=100601.667\tan(2\theta_p) = \frac{2 \times 50}{80 - 20} = \frac{100}{60} \approx 1.667

2θptan1(1.667)59.042\theta_p \approx \tan^{-1}(1.667) \approx 59.04^\circ θp59.04229.52\theta_p \approx \frac{59.04^\circ}{2} \approx 29.52^\circ

This angle θp\theta_p is the orientation of the principal stresses with respect to the original x-axis.

The angle θs\theta_s for maximum shear stress (in physical space) is: θs=θp+4529.52+45=74.52\theta_s = \theta_p + 45^\circ \approx 29.52^\circ + 45^\circ = 74.52^\circ

Summary of Results:

  • Principal stresses: σ1=108.31\sigma_1 = 108.31 MPa, σ2=8.31\sigma_2 = -8.31 MPa
  • Maximum shear stress: τmax=58.31\tau_{\text{max}} = 58.31 MPa
  • Direction of principal stresses: θp29.52\theta_p \approx 29.52^\circ (counterclockwise from the x-axis)
  • Direction of maximum shear stress: θs74.52\theta_s \approx 74.52^\circ (counterclockwise from the x-axis)

Would you like a more detailed explanation, or do you have any questions about the process?

Related Questions:

  1. How would the principal stresses change if σy\sigma_y was negative?
  2. Can you explain how the direction of the principal stresses relates to the original stress element?
  3. What is the significance of Mohr's circle in stress analysis?
  4. How would the result change if τxy\tau_{xy} was counterclockwise instead of clockwise?
  5. Can Mohr's circle be used to find the principal strains? How?

Tip:

When working with Mohr's circle, always pay close attention to the sign conventions for stresses, as they directly affect the position and orientation of the circle and the resulting principal stresses.

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Math Problem Analysis

Mathematical Concepts

Mechanics of Materials
Stress Analysis
Mohr's Circle

Formulas

Mohr's Circle equations

Theorems

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Suitable Grade Level

Advanced Engineering