Question 4 of 8: Propped Beam: Strut Buckling Sets the Maximum Load
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
EGBC National Exam — Basic Studies, 04-BS-6 Mechanics of Materials, 2018-Dec. Closed book; one hand-written aid sheet permitted. The exam instructs "any FIVE of the eight questions constitute a complete paper," but every question is solved below as a full study resource.
Reference texts: Hibbeler, Mechanics of Materials, 10th ed. (axial deformation & statically indeterminate assemblies ch.4; shear/moment diagrams ch.6; stress transformation & Mohr's circle ch.9; buckling of columns ch.13; torsion of circular shafts ch.5; transformed-section composite beams ch.6; shear flow/VQ/Ib ch.7; beam deflection by integration ch.9). Standard steel W-shape tables (Appendix C of the exam) per CISC Handbook of Steel Construction.
Question 4: Propped Beam: Strut Buckling Sets the Maximum Load (20 marks)
Given. Beam $AB$: pinned to the wall at $A$, horizontal, length $L=6\text{ m}$, carrying UDL $w$ (to be found) over its full length. Strut $BC$: pinned at both ends, $60\times60\text{ mm}$ square, $\sigma_Y=500\text{ MPa}$, $E=200\text{ GPa}$; from B, C is $2\text{ m}$ horizontally and $3\text{ m}$ vertically down. Buckling factor of safety $=2$; no yield safety factor applied.
Find. The maximum UDL $w$ the beam can carry, governed by Euler buckling of the strut.
Beam AB (UDL w) propped by inclined strut BC; buckling of the pin-pin strut governs the maximum w.
Approach. Free-body the beam AB alone (pin reactions at A, axial strut force at B); take moments about A to express the strut force in terms of w, then set that force equal to the Euler critical load of the strut divided by the given factor of safety and solve for w.
Moment equilibrium of beam AB about A. The strut is a two-force (pin-pin) member, so its force $S$ (compression) acts on the beam at B along the strut axis; only its VERTICAL component ($S\cdot3/L_{strut}$, since B is at the same height as A) creates moment about A. Setting the strut moment equal to the UDL's moment: $S\left(\dfrac{3}{L_{strut}}\right)(6)=w(6)(3)\Rightarrow S=\dfrac{w\,L\,L_{strut}}{2(3)}=w(3.606)\text{ kN per kN/m of }w$.
Euler buckling load of the strut ($K=1$, pin-pin). $I=\dfrac{60^4}{12}=1.08\times10^{6}\text{ mm}^4$; $P_{cr}=\dfrac{\pi^2EI}{L_{strut}^2}=\dfrac{\pi^2(200{,}000)(1.08\times10^6)}{3{,}605.55^2}=\boxed{163{,}987\text{ N}}=163.99\text{ kN}$.
Allowable strut force and solve for w. $S_{allow}=P_{cr}/\text{FS}=163.99/2=\boxed{81.99\text{ kN}}$. Setting $S=S_{allow}$: $w_{max}=81.99/3.606=\boxed{22.74\text{ kN/m}}$.
Confirm buckling (not yield) governs. At $w_{max}$, the strut stress is $\sigma=S_{allow}/(60\times60)=81{,}990/3{,}600=22.8\text{ MPa}$, far below $\sigma_Y=500\text{ MPa}$ — consistent with the problem statement that no yield safety factor is needed, since buckling of this slender strut governs the design by a wide margin.