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04-BS-6 · May 2013

Question 3 of 8: Two-rod truss — Euler buckling capacity

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

Notes on this paper

National Exams — May 2013 — 04-BS-6 Mechanics of Materials. Three-hour, closed-book exam (one double-sided hand-written aid sheet permitted, approved Casio/Sharp calculator only). Format: eight questions offered; any five constitute a complete paper and only the first five appearing in the answer book are marked. All eight are solved below for completeness. No credit is given in the original exam for solutions built by superposing existing standard solutions on Questions 1 and 6 — both are solved here by direct integration/equilibrium as required.

Reference texts: Hibbeler, Mechanics of Materials (10th ed., Pearson) — beam deflection by integration (Ch. 12), stress transformation and Mohr's circle (Ch. 9), columns and buckling (Ch. 13), combined axial & bending loading (Ch. 8), torsion of circular shafts (Ch. 5), transformed-section method for composite beams (Ch. 6), shear and moment diagrams (Ch. 6-7); Beer, Johnston & DeWolf, Mechanics of Materials (7th ed., McGraw-Hill) — cross-check reference for the same topics.

sigmatauX (20,20)Y (-10,-20)sigma1=30sigma2=-20Q2: Mohr's circle (C=5, R=25 MPa)
Mohr's circle: center (5,0) MPa, radius 25 MPa.

Question 3: Two-rod truss — Euler buckling capacity (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.

ABCP45°4 m3 m4 mQ3: truss ABC (rods AB, BC)
Truss geometry: A (wall pin), B (free joint), C (ground pin); load P at 45° from vertical.

Given.

QuantityValue
$L_{AB}$ (4 m horiz., 3 m vert.)5 m
$L_{BC}$ (vertical)4 m
Rod diameter120 mm (both rods, pinned both ends)
$F_y$, $E$350 MPa, 200 GPa
Euler safety factor2 (no SF on yielding)

Find. The largest load $P$ the truss can support.

Approach. Solve joint B for the member forces in terms of $P$, then compare each member's actual compressive force against its lesser of (i) yield capacity $F_yA$ and (ii) allowable Euler load $\pi^2EI/(KL)^2\big/2$ (pin-ended, $K=1$); the governing member sets $P_{max}$.

  1. Joint equilibrium at B. Unit vectors: $\hat u_{BA}=(-0.8,0.6)$, $\hat u_{BC}=(0,-1)$. With $P$ applied at $45^\circ$ from vertical, down-left: $P_x=-P\sin45^\circ$, $P_z=-P\cos45^\circ$. Solving $T_{AB}\hat u_{BA}+T_{BC}\hat u_{BC}+\vec P=0$: $$T_{AB}=-0.8839\,P,\qquad T_{BC}=-1.2374\,P$$ Both are negative — both rods are in compression for any positive $P$, so both must be checked for buckling.
  2. Section and Euler loads. $A=\pi(60)^2=11\,309.7\ \text{mm}^2$, $I=\pi(60)^4/4=1.01788\times10^{7}\ \text{mm}^4$. $$P_{cr,AB}=\frac{\pi^2EI}{L_{AB}^2}=\frac{\pi^2(200\,000)(1.01788\times10^7)}{5000^2}=803.7\ \text{kN},\qquad P_{cr,BC}=\frac{\pi^2EI}{L_{BC}^2}=1255.8\ \text{kN}$$
  3. Allowable compressive load per member. Yield capacity $F_yA=350(11\,309.7)=3958.4$ kN is far above either Euler load, so buckling governs both members: $$P_{allow,AB}=\frac{P_{cr,AB}}{2}=401.8\ \text{kN},\qquad P_{allow,BC}=\frac{P_{cr,BC}}{2}=627.9\ \text{kN}$$
  4. Back out the governing applied load. Using the force coefficients from Step 1: $$P\big|_{AB\ \text{limit}}=\frac{401.8}{0.8839}=454.6\ \text{kN},\qquad P\big|_{BC\ \text{limit}}=\frac{627.9}{1.2374}=507.4\ \text{kN}$$ Member AB reaches its Euler-buckling limit first, so $$P_{max}=\boxed{454.6\ \text{kN}}$$
QuantityResult
$T_{AB}$, $T_{BC}$ (at $P_{max}$)−401.8 kN, −562.6 kN (both compression)
Governing modeEuler buckling of AB (SF = 2)
$P_{max}$454.6 kN
-2600 N.m (AB)200 N.m (BC)-1800 N.m (at C+)Q8: internal torque diagram T(x)
Internal torque diagram T(x) (CCW positive).