NivaarExam PrepOfficial exam papers ↗

22-Mec-A7 Advanced Strength of Materials · December 2013

Question 2 of 7: Plane-Stress Square Plate — Inverse Determination

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

Notes on this paper

Paper format: National Exams, December 2013 — 07-Mech-A7 Advanced Strength of Materials. Open-book, 3 hours; any five of the seven problems constitute a complete paper and all problems are of equal value. All seven problems are solved as a study resource.

Reference texts. R.C. Hibbeler, Mechanics of Materials, 10th ed. (thermal & indeterminate axial members Ch. 4, plane stress/strain Ch. 9–10, energy methods Ch. 14); A.P. Boresi & R.J. Schmidt, Advanced Mechanics of Materials, 6th ed. (thick-walled cylinders Ch. 11, thin-walled open sections & torsional buckling Ch. 6&12); J.M. Gere & B.J. Goodno, Mechanics of Materials (strain rosettes, columns). Yield criteria follow the von Mises and Tresca formulations standard to these texts.

Question 2: Plane-Stress Square Plate — Inverse Determination (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 2 m square plate in biaxial plane stress with measured edge elongations and one known stress.

Given data
Plate size2 m × 2 m (L = 2000 mm each side)
Elongationsδx = 0.8 mm ⇒ εx = 4.0×10−4; δy = 0.2 mm ⇒ εy = 1.0×10−4
Known stress / modulusσy = 200 MPa, E = 80 GPa
Stress stateσz = τ = 0 (plane stress)

Find. (a) σx; (b) ν; (c) εz.

σx σy
Biaxial plane stress; σx tensile (horizontal), σy = 200 MPa tensile (vertical).

Approach. Two biaxial Hooke’s-law equations relate (εx, εy) to (σx, ν) with σy and E known. Eliminating σx leaves a quadratic in ν; the thickness strain then follows from the plane-stress form of εz.

  1. Biaxial Hooke’s law. With Eε written out, $$E\varepsilon_x=\sigma_x-\nu\sigma_y=32\ \text{MPa},\qquad E\varepsilon_y=\sigma_y-\nu\sigma_x=8\ \text{MPa}.$$
  2. Eliminate σx. From the first equation σx = 32 + 200ν; substituting into the second, $$\nu(32+200\nu)=192\ \Longrightarrow\ 25\nu^{2}+4\nu-24=0.$$
  3. Solve for ν (part b). The positive root is $$\boxed{\nu=\frac{-4+\sqrt{16+2400}}{50}=0.903.}$$
  4. Back-substitute for σx (part a). $$\boxed{\sigma_x=32+200(0.903)=212.6\ \text{MPa}.}$$
  5. Thickness strain (part c). In plane stress the out-of-plane strain is $$\varepsilon_z=-\frac{\nu}{E}\,(\sigma_x+\sigma_y)=-\frac{0.903}{80\,000}(212.6+200)=\boxed{-4.66\times10^{-3}.}$$

Check — data inconsistency. The measured elongations force ν = 0.903, which exceeds the isotropic upper bound ν < 0.5 (an isotropic material with ν → 0.5 is incompressible; ν > 0.5 gives a negative bulk modulus). The given δx, δy, σy and E are therefore not mutually consistent for a real isotropic plate — a data flaw in the printed exam. Following the exam’s “state your assumptions” rubric, the algebra is carried through as posed (the method is what is examined); the numerical ν and εz should be reported with the note that they are non-physical. Had δy been, say, 0.35 mm, the data would return an admissible ν ≈ 0.28.

Results — Question 2 (as-given data)
QuantityValue
σx212.6 MPa (tension)
Poisson’s ratio ν0.903 (inadmissible — see note)
Thickness strain εz−4.66×10−3