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22-Mec-A7 Advanced Strength of Materials · December 2018

Question 7 of 8: Joint displacement of a three-element truss (Castigliano / virtual work)

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

Notes on this paper

Paper format. National Exams, December 2018 — 16-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours. Eight problems of equal value; any five constitute a complete paper. All eight problems are solved as a study resource.

Reference texts. Boresi & Schmidt, Advanced Mechanics of Materials (6th ed.); Ugural & Fenster, Advanced Strength and Applied Elasticity (5th ed.); Hibbeler, Mechanics of Materials (10th ed.); Timoshenko & Goodier, Theory of Elasticity (3rd ed.).

Question 7: Joint displacement of a three-element truss (Castigliano / virtual work) (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. Three pin-jointed members meet at the loaded joint B; their far ends A, C, D are pinned to supports.

Given data (from the figure)
Geometry$a=0.75$ m (horizontal A–B), $b=0.90$ m (vertical B–D)
Member ABhorizontal, $L=0.75$ m
Member BDvertical, $L=0.90$ m
Member CBdiagonal, $L=\sqrt{0.75^2+0.90^2}=1.172$ m
Section area$A=5\text{ cm}^2=5\times10^{-4}$ m$^2$ (all)
Modulus $E$200 GPa
Load at B16 000 N, 30° above horizontal, up-and-right
A B C D P = 16 kN a = 0.75 m b = 0.90 m
Three-element truss: joint B connects horizontal AB, vertical BD and diagonal CB to fixed supports A, C, D. Load P = 16 kN acts 30° above horizontal.

Find. Horizontal ($u$) and vertical ($v$) displacement of joint B.

Approach. Joint B is the only free node; each member ties it to a fixed support, so B behaves like a mass on three axial springs. Assemble the 2×2 joint stiffness $\mathbf K=\sum(EA/L)\,\hat{\mathbf n}\hat{\mathbf n}^{\mathsf T}$ and solve $\mathbf K\{u,v\}=\mathbf P$. This is equivalent to a unit-load (Castigliano) evaluation but collapses the bookkeeping.

  1. Unit vectors from B to each support. Taking B at the origin, right/up positive: to A $(-1,0)$, to D $(0,-1)$, to C $(-0.640,-0.768)$.
  2. Member axial stiffnesses. $EA=200\times10^9\times5\times10^{-4}=1.0\times10^{8}$ N; then $EA/L$ = $1.333\times10^{8}$ (AB), $1.111\times10^{8}$ (BD), $8.536\times10^{7}$ N/m (CB).
  3. Assemble K. Summing $(EA/L)\,\hat{\mathbf n}\hat{\mathbf n}^{\mathsf T}$, $$\mathbf K=\begin{bmatrix}1.683\times10^{8} & 4.198\times10^{7}\\[2pt] 4.198\times10^{7} & 1.615\times10^{8}\end{bmatrix}\ \tfrac{\text{N}}{\text{m}}.$$
  4. Load vector and solve. $\mathbf P=(16\,000\cos30^\circ,\,16\,000\sin30^\circ)=(13\,856,\,8\,000)$ N. Then $$\{u,v\}=\mathbf K^{-1}\mathbf P\;\Rightarrow\;\boxed{u_B=0.075\text{ mm (right)},\quad v_B=0.030\text{ mm (up)}}.$$
Final results — Question 7
ComponentValue
Horizontal $u_B$0.075 mm (rightward)
Vertical $v_B$0.030 mm (upward)