22-Mec-A7 Advanced Strength of Materials · May 2018
Question 1 of 8: Displacement of a Three-Bar Truss
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2018 — 16-Mec-A7 Advanced Strength of Materials. Open-book, 3 hours, eight problems of equal value; a complete paper is any five. All eight problems are solved here as a study resource.
Reference texts. Boresi & Schmidt, Advanced Mechanics of Materials (6th); Ugural & Fenster, Advanced Mechanics of Materials and Applied Elasticity (5th); Timoshenko & Goodier, Theory of Elasticity (3rd); Hibbeler, Mechanics of Materials (10th).
Question 1: Displacement of a Three-Bar Truss (20 marks)
Q1. Three bars AB (horizontal), BD (vertical) and BC (diagonal) meet at the single free joint B; A is a wall pin, C a ground pin and D a roller. P acts along BC, directed away from C (up and to the right).
Given. Three pin-ended bars meet at the one free joint B; their far ends A, C and D are held by fixed supports, and the 7000 N load acts along line BC.
Given data
Applied force
$P = 7000\ \text{N}$, co-linear with BC (up–right)
Find. Horizontal displacement $u_B$ and vertical displacement $v_B$ of joint B.
Approach. Only joint B can move and three bars run to fixed supports, so the joint is statically indeterminate to the first degree. The cleanest energy route writes the strain energy in the two joint displacements and stationarizes it, giving a $2\times2$ joint-stiffness relation $\mathbf{K}\,\boldsymbol{\delta}=\mathbf{F}$ (Castigliano’s second theorem applied at the joint).
Member directions and lengths. With B at the origin, the unit vectors from B toward each support and the lengths are $\hat{n}_{BA}=(-1,0),\ L=0.50\,\text{m}$; $\hat{n}_{BD}=(0,-1),\ L=0.60\,\text{m}$; $\hat{n}_{BC}=(-0.6402,-0.7682),\ L=0.781\,\text{m}$.
Axial stiffness of each bar. $k_i=\dfrac{AE}{L_i}$ with $AE=750\times10^{-6}\cdot70\times10^{9}=5.25\times10^{7}\ \text{N}$: $k_{BA}=1.050\times10^{8}$, $k_{BD}=8.750\times10^{7}$, $k_{BC}=6.722\times10^{7}\ \text{N/m}$.
Assemble the joint stiffness. Each bar contributes $k_i\,\hat{n}_i\hat{n}_i^{\mathsf T}$, so $$\mathbf{K}=\sum_i k_i\begin{bmatrix}c_i^2&c_is_i\\c_is_i&s_i^2\end{bmatrix}=\begin{bmatrix}13.26&3.306\\3.306&12.72\end{bmatrix}\times10^{7}\ \text{N/m}.$$
Load components at B. The unit vector from C to B is $(0.6402,\ 0.7682)$, so $F_x=7000(0.6402)=4481\ \text{N}$ and $F_y=7000(0.7682)=5378\ \text{N}$ (both positive).
Solve for the joint displacement. Inverting $\mathbf{K}\{u_B,v_B\}^{\mathsf T}=\{F_x,F_y\}^{\mathsf T}$ gives $$\boxed{u_B = 0.0249\ \text{mm}\ (\rightarrow),\qquad v_B = 0.0358\ \text{mm}\ (\uparrow)}$$
Physical check. The load pulls B up and to the right, away from all three supports, so every bar is in tension and B displaces a small amount into the load quadrant — consistent with both components coming out positive.