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04-BS-6 · May 2014

Question 4 of 8: Maximum Load on a Beam Propped by a Buckling Strut

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

Notes on this paper

National Exams May 2014 – 04-BS-6: Mechanics of Materials
3 hours duration, closed book (one hand-written aid sheet permitted). Any five of the eight questions constitute a complete paper; all eight are solved below as a complete study resource.

Reference texts: R.C. Hibbeler, Mechanics of Materials, 10th ed. (Ch. 5 torsion, Ch. 6 shear/moment diagrams & composite beams, Ch. 7 transverse shear, Ch. 8 combined loadings, Ch. 9 stress transformation, Ch. 12 deflection by integration, Ch. 13 buckling); F. Beer & E.R. Johnston, Mechanics of Materials; W. Gere & B. Goodno, Mechanics of Materials (alternates). A wide-flange (W-shape) properties table printed on the exam's last page supplies the section used in Question 8.

Question 4: Maximum Load on a Beam Propped by a Buckling Strut (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.

wABC6 m2 m4 mFig. Q4 – propped beam AB, pinned strut BC (buckling)
Beam AB (6 m, UDL w) pinned at A, propped by strut BC (2 m horizontal, 4 m vertical offset), 80×80 mm section, pinned both ends.

Given.

QuantityValue
Beam length AB6 m, pinned at A
Strut offsets (B to C)2 m horizontal, 4 m vertical
Strut section80 mm × 80 mm, pinned both ends
Strut E, fy200 GPa, 350 MPa
Factor of safety on buckling2 (no safety factor on yield)

Find. The maximum UDL w the beam can carry before the strut buckles.

Approach. The pin-pin strut BC is a two-force member, so its Euler buckling capacity (divided by the FS) sets the maximum axial force it may carry; resolve that force into its vertical component acting on the beam at B, then use moment equilibrium of beam AB about A to convert that into the maximum w.

  1. Strut geometry and section. $$L_{BC} = \sqrt{2000^2+4000^2} = 4472\ \text{mm}, \qquad I = \frac{80(80)^3}{12} = 3.413\times10^6\ \text{mm}^4$$
  2. Euler buckling capacity. Pinned-pinned, K = 1: $$P_{cr} = \frac{\pi^2EI}{L^2} = \frac{\pi^2(200{,}000)(3.413\times10^6)}{4472^2} = 336.9\ \text{kN}$$ $$P_{allow} = \frac{P_{cr}}{FS} = \frac{336.9}{2} = \boxed{168.4\ \text{kN}}$$
  3. Moment equilibrium of beam AB about A. The strut force $F$ acts on the beam at B along the strut's own line, with vertical component fraction $v_{off}/L_{BC}=4000/4472=0.8944$; the UDL resultant $wL_{beam}$ acts at $L_{beam}/2$: $$F\!\left(\frac{v_{off}}{L_{BC}}\right)L_{beam} = wL_{beam}\!\left(\frac{L_{beam}}{2}\right) \ \Rightarrow\ w = \frac{2F(v_{off}/L_{BC})}{L_{beam}}$$
  4. Maximum w at the strut's allowable load. Setting $F=P_{allow}=168.4$ kN: $$\boxed{w_{max} = \frac{2(168.4)(0.8944)}{6} = 50.2\ \text{kN/m}}$$

Final Results.

QuantityValue
LBC, Istrut4472 mm, 3.413 × 106 mm4
Pcr (Euler)336.9 kN
Pallow = Pcr/FS168.4 kN
Maximum UDL w50.2 kN/m