Question 6 of 8: Beam with an Inclined Cable — Combined Axial + Bending
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams December 2015 — 04-BS-6: Mechanics of Materials (3 hours, closed book,
one hand-written aid sheet permitted). Any FIVE of the eight questions constitute a complete paper on the official exam; every question is answered below.
Reference texts: Hibbeler, Mechanics of Materials, 10th ed. (beam
deflection, torsion, transformation of stress, combined loading, columns); CISC Handbook of
Steel Construction (W-shape section properties, attached to this exam).
Question 6: Beam with an Inclined Cable — Combined Axial + Bending (20 marks, 4 bonus)
inclined, +1.5 m horizontal, +2 m vertical to its anchor (length 2.5 m; 3-4-5 triangle)
Section
Symmetric I: bf=100 mm, tf=15 mm, tw=20 mm, d=300 mm
Steel
σY=350 MPa, τY=60 MPa, E=200 GPa
Beam AB: pin at A, full-span UDL, and an inclined cable at B running up and away from A.
Find. Normal-stress distribution (max/min) and maximum shear stress at x=1 m
from A; the plastic moment capacity.
Approach. Because the cable is inclined, it pulls B both up and toward
the wall; the pin at A must react that horizontal pull, which puts the whole beam into constant
axial tension — so this is a combined axial-plus-bending problem, not pure bending. Solve
reactions (including the cable's horizontal component), get the section forces at x=1 m, then
superpose $\sigma = N/A \pm Mc/I$.
Cable tension and reactions. With $\cos\alpha=1.5/2.5=0.6,\ \sin\alpha=0.8$,
moments about A ($w L\cdot L/2$ balanced by the cable's vertical component at B):
$$T\sin\alpha\,L = wL\cdot\frac{L}{2} \;\Rightarrow\; T = \frac{60(4)/2}{0.8} = 150\ \text{kN}$$
$$T_x=90\ \text{kN},\quad T_y=120\ \text{kN},\quad A_y = wL-T_y = 240-120=120\ \text{kN}$$
Axial force in the beam. The pin reacts the cable's horizontal pull,
$A_x=-T_x=-90$ kN; tracing this through the beam (cable pulls B toward the wall, pin holds A back)
puts the ENTIRE beam in constant axial tension:
$$\boxed{N = 90\ \text{kN (tension), constant along AB}}$$
Section forces at x = 1 m (only the UDL and $A_y$ act to the left of the cut):
$$M(1\text{m}) = A_y(1000)-\frac{w(1000)^2}{2} = 120{,}000(1000)-\frac{60(1000)^2}{2}=90.0\times10^6\ \text{N}\cdot\text{mm}$$
$$V(1\text{m}) = A_y - w(1000) = 120-60=60\ \text{kN}$$
Superpose axial and bending stress ($N/A$ tension is uniform; the sagging
moment puts the top in compression, the bottom in tension):
$$\sigma_{top} = \frac{N}{A}-\frac{Mc}{I} = 10.71-143.96 = \boxed{-133.2\ \text{MPa (compression, top)}}$$
$$\sigma_{bot} = \frac{N}{A}+\frac{Mc}{I} = 10.71+143.96 = \boxed{+154.7\ \text{MPa (tension, bottom)}}$$
Both stay under the 350 MPa yield.
Maximum shear stress at the neutral axis, $Q_{NA}=1500(142.5)+2700(67.5)=3.96\times10^5\ \text{mm}^3$:
$$\boxed{\tau_{max} = \frac{VQ_{NA}}{I\,t_w} = \frac{60{,}000(3.96\times10^5)}{9.378\times10^7(20)} = 12.67\ \text{MPa}} \quad(\ll 60\ \text{MPa yield})$$
Bonus (c): plastic moment capacity of the section, $Z=b_ft_f(d-t_f)+t_w(d-2t_f)^2/4$:
$$Z = 100(15)(285)+20\frac{(270)^2}{4}=792{,}000\ \text{mm}^3 \;\Rightarrow\; \boxed{M_p = \sigma_Y Z = 350(792{,}000) = 277.2\ \text{kN}\cdot\text{m}}$$
Normal-stress distribution at x = 1 m: compression at top, tension at bottom, shifted by the constant axial tension.