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22-Mec-A7 Advanced Strength of Materials · December 2016

Question 6 of 8: Biaxial stresses in a thin plate and factor of safety

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

National Exams — December 2016 · 07-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours. Eight problems of equal value; any five constitute a complete paper. All eight are solved as a study resource.

Reference texts. Boresi & Schmidt, Advanced Mechanics of Materials, 6th ed.; Ugural & Fenster, Advanced Strength and Applied Elasticity, 4th ed.; Hibbeler, Mechanics of Materials, 10th ed.; Timoshenko & Gere, Theory of Elastic Stability.

Check: the figure for Question 1 labels the applied load P = 7000 N, whereas the printed text reads “7800 N”. The drawn value on the exam figure governs, so 7000 N is used throughout.

Question 6: Biaxial stresses in a thin plate and factor of safety (20 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. A thin plate in biaxial plane stress; the two edge elongations are measured and the elastic constants are known.

Given data
Plate size1.5 m × 1.5 m
x-elongationδx = 0.8 mm → εx = 5.333×10−⁴
y-elongationδy = 0.25 mm → εy = 1.667×10−⁴
Elastic constantsE = 120 GPa, v = 0.28

Find. (a) $\sigma_x,\sigma_y$ from the measured strains; (b) the factor of safety by the maximum-shear-stress theory.

Approach. Invert the plane-stress Hooke’s law to get the stresses from the two strains, then form the principal stresses and apply Tresca for the factor of safety.

  1. (a) Invert plane-stress Hooke. With $\sigma_x=\dfrac{E(\varepsilon_x+v\varepsilon_y)}{1-v^2}$ and $\sigma_y=\dfrac{E(\varepsilon_y+v\varepsilon_x)}{1-v^2}$ (using $1-v^2=0.9216$): $$\boxed{\sigma_x=75.5\ \text{MPa},\qquad \sigma_y=41.1\ \text{MPa.}}$$
  2. Principal stresses. The stresses are already principal (no shear): $\sigma_1=75.5$, $\sigma_2=41.1$, $\sigma_3=0$ MPa (the out-of-plane direction). Maximum shear $\tau_{max}=(\sigma_1-\sigma_3)/2=37.8$ MPa.
  3. (b) Factor of safety (Tresca). The maximum-shear theory gives $N=\dfrac{\sigma_Y}{\sigma_1-\sigma_3}=\dfrac{\sigma_Y}{75.5\ \text{MPa}}$. The plate’s yield strength is not stated; for a representative structural value $\sigma_Y=250$ MPa, $$\boxed{N=\sigma_Y/75.5\ \text{MPa}\approx3.3.}$$
Check: Question 6 gives no yield strength, yet asks for a numerical factor of safety. The FoS is therefore reported as the exact ratio $\sigma_Y/75.5\ \text{MPa}$; the value 3.3 assumes a representative $\sigma_Y=250$ MPa (mild steel). Substitute the intended yield strength to finalize.
Final results — Q6
QuantityValue
σx75.5 MPa
σy41.1 MPa
τmax37.8 MPa
Factor of safety (Tresca)σY/75.5 MPa (≈ 3.3 at σY = 250 MPa)