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

Question 2 of 8: Two-Segment Rod — Thermal Stress in a Statically Indeterminate Bar

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

Notes on this paper

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

Reference texts: A. C. Ugural & S. K. Fenster, Advanced Strength and Applied Elasticity, 4th ed.; A. P. Boresi & R. J. Schmidt, Advanced Mechanics of Materials, 6th ed.; R. C. Hibbeler, Mechanics of Materials, 10th ed.; S. P. Timoshenko & J. M. Gere, Theory of Elastic Stability, 2nd ed.

Question 2: Two-Segment Rod — Thermal Stress in a Statically Indeterminate Bar (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 composite rod A–B–C built in between two rigid walls, heated uniformly by ΔT = 50 °C.

Given data
Rod (1) A–BE1 = 180 GPa, A1 = 550 mm2, L1 = 150 mm, α1 = 8×10−6/°C
Rod (2) B–CE2 = 90 GPa, A2 = 900 mm2, L2 = 100 mm, α2 = 17×10−6/°C
Temperature riseΔT = +50 °C

Find. (a) the axial stress in each rod; (b) the direction and magnitude of the displacement of joint B.

(1) (2) A B C rigidrigid
Two welded rods restrained between rigid walls; the same internal force N passes through both segments.

Approach. The rigid walls prevent any net length change, so a single internal force N (constant through the series) develops such that the combined mechanical + thermal elongation is zero. Solve the compatibility equation for N, divide by area for stress, then integrate the elongation of segment (1) to locate B.

  1. Compatibility. Zero total change in length between the fixed walls: $$\delta_{tot}=\Big(\tfrac{NL_1}{A_1E_1}+\alpha_1L_1\Delta T\Big)+\Big(\tfrac{NL_2}{A_2E_2}+\alpha_2L_2\Delta T\Big)=0.$$
  2. Solve for the internal force. Rearranging, $$N=-\frac{\Delta T\,(\alpha_1L_1+\alpha_2L_2)}{\dfrac{L_1}{A_1E_1}+\dfrac{L_2}{A_2E_2}}=-\frac{50(1.20+1.70)\times10^{-3}}{(1.515+1.235)\times10^{-6}}.$$ $$\boxed{N=-52.73\ \text{kN}\quad(\text{compression})}$$
  3. Axial stresses. Same force, different areas: $$\sigma_1=\frac{N}{A_1}=\frac{-52\,733}{550}=-95.9\ \text{MPa},\qquad \sigma_2=\frac{N}{A_2}=\frac{-52\,733}{900}=-58.6\ \text{MPa}.$$ Both rods are in compression, as expected for restrained heating.
  4. Displacement of joint B. B moves by the actual elongation of segment (1) measured from wall A: $$u_B=\frac{NL_1}{A_1E_1}+\alpha_1L_1\Delta T=(-0.0799)+(0.0600)=-0.0199\ \text{mm}.$$ $$\boxed{u_B \approx 0.020\ \text{mm to the left (toward A)}}$$ The check from the C–side, $-(NL_2/A_2E_2+\alpha_2L_2\Delta T)=-0.0199$ mm, agrees.
Question 2 — results
QuantityValue
Internal force N52.73 kN (compression)
Stress σ1−95.9 MPa
Stress σ2−58.6 MPa
Movement of B0.020 mm to the left