22-Mec-A7 Advanced Strength of Materials · May 2015
Question 1 of 8: Displacements of a Pin-Jointed Truss Joint
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, May 2015 — 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 here.
Reference texts. Ugural & Fenster, Advanced Strength and Applied Elasticity (4th ed.); Boresi & Schmidt, Advanced Mechanics of Materials (6th ed.); Hibbeler, Mechanics of Materials (10th ed.); Timoshenko & Goodier, Theory of Elasticity.
Question 1: Displacements of a Pin-Jointed Truss Joint (20 marks)
Given. A three-bar truss with the free (loaded) joint B restrained by three pinned members meeting at B.
Given data
Horizontal load at B, P
38 000 N (→)
Member area, A
9 cm2 = 900 mm2
Panel width, a
80 cm = 0.80 m
Panel height, b
100 cm = 1.00 m
Young’s modulus, E
180 GPa
Find. The horizontal displacement u and vertical displacement v of joint B.
Truss: member AB (horizontal), CB (diagonal) and DB (vertical) all pinned to fixed supports; only joint B is free.
Approach. Joint B carries three members but offers only two equilibrium equations, so the truss is statically indeterminate to the first degree; solve by the direct-stiffness (displacement) method using the two unknown displacements (u, v) at B.
Set geometry and direction cosines. With A(0, 0), B(0.8, 0), C(0, −1.0), D(0.8, −1.0) m, the unit vectors from each support toward B are $$\text{AB}:(c,s)=(1,0),\ L=0.80;\quad \text{CB}:(0.625,0.781),\ L=1.281;\quad \text{DB}:(0,1),\ L=1.00.$$ The axial rigidity is $EA=180\times10^{9}\times900\times10^{-6}=1.62\times10^{8}\ \text{N}$.
Assemble the joint stiffness. Each bar contributes $k_i=\dfrac{EA}{L_i}\begin{bmatrix}c^2&cs\\cs&s^2\end{bmatrix}$, so $$K=\sum_i k_i=\begin{bmatrix}2.519\times10^{8}&6.171\times10^{7}\\[2pt]6.171\times10^{7}&2.391\times10^{8}\end{bmatrix}\ \text{N/m}.$$
Solve the joint equilibrium. With the applied load $\{F\}=\{38\,000,\,0\}^{\mathsf T}$ N, solving $K\{u,v\}^{\mathsf T}=\{F\}$ gives $$\boxed{u=+0.161\ \text{mm (right)},\qquad v=-0.0416\ \text{mm (down)}.}$$ The horizontal displacement dominates because member AB is aligned with the load; the small downward v arises from the flexibility of the inclined member CB.