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)
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.
Quantity
Value
Beam length AB
6 m, pinned at A
Strut offsets (B to C)
2 m horizontal, 4 m vertical
Strut section
80 mm × 80 mm, pinned both ends
Strut E, fy
200 GPa, 350 MPa
Factor of safety on buckling
2 (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.
Strut geometry and section.
$$L_{BC} = \sqrt{2000^2+4000^2} = 4472\ \text{mm}, \qquad
I = \frac{80(80)^3}{12} = 3.413\times10^6\ \text{mm}^4$$
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 $L_{beam}/2$:
$$F\!\left(\frac{v_{off}}{L_{BC}}\right)L_{beam} = wL_{beam}\!\left(\frac{L_{beam}}{2}\right)
\ \Rightarrow\ w = \frac{2F(v_{off}/L_{BC})}{L_{beam}}$$
Maximum w at the strut's allowable load. Setting $F=P_{allow}=168.4$ kN:
$$\boxed{w_{max} = \frac{2(168.4)(0.8944)}{6} = 50.2\ \text{kN/m}}$$