22-Mec-A7 Advanced Strength of Materials · May 2016
Question 4 of 8: Inverse plane-stress problem for a square plate
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format: National Exams — May 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. A.P. Boresi & R.J. Schmidt, Advanced Mechanics of Materials, 6th ed. (Wiley); A.C. Ugural & S.K. Fenster, Advanced Strength and Applied Elasticity, 4th ed. (Prentice Hall); R.C. Hibbeler, Mechanics of Materials, 10th ed. (Pearson); J.M. Gere & B.J. Goodno, Mechanics of Materials, 9th ed. All symbols follow the paper’s notation.
Question 4: Inverse plane-stress problem for a square plate (equal value)
Given. Side L = 1.25 m = 1250 mm; elongations Δx = 1.95 mm, Δy = 0.20 mm, so εx = 1.56 × 10−3, εy = 1.6 × 10−4; σx = 200 MPa; E = 110 GPa; plane stress (σz = 0).
Find. (a) σy and ν; (b) the yield strength under Tresca.
Approach. The two plane-stress Hooke’s-law equations contain the two unknowns σy and ν. Eliminating σy gives a quadratic in ν; keep the admissible root (ν < 0.5). Then apply Tresca to the resulting principal stresses.
Plane-stress Hooke’s law.
$$E\varepsilon_x=\sigma_x-\nu\sigma_y=171.6,\qquad E\varepsilon_y=\sigma_y-\nu\sigma_x=17.6$$
From the first, νσy = 28.4 MPa; from the second, σy = 17.6 + 200ν.
Back-substitute for σy.
$$\sigma_y=17.6+200(0.335)=84.7\ \text{MPa}\quad(\text{check: }\nu\sigma_y=28.4\ \checkmark)$$
$$\boxed{\sigma_y=84.7\ \text{MPa}}$$
Tresca yield strength (part b). The principal stresses are σ1 = 200, σ2 = 84.7, σ3 = 0 (out-of-plane). Maximum shear governs on the largest difference:
$$\sigma_Y=\sigma_1-\sigma_3=200-0 \;\Rightarrow\; \boxed{\sigma_Y=200\ \text{MPa}}$$