24-Bld-A1 Elementary Structural Analysis · December 2017
Question 6 of 8: Slope-deflection analysis of a propped frame with a cantilever overhang (22 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams December 2017 — 07-BLD-A1 Elementary Structural Analysis, 3 hours, closed book. Answer ALL of Questions 1–5; answer ONLY ONE of Questions 6, 7 or 8 (this solution set, per pipeline convention, answers all three optional questions).
Given. Fixed support at 2 (x=0); horizontal member 2–3 ($$3EI$$, 6 m); a 3 m vertical strut ($$EI$$) from joint 3 down to a pin support at 1; horizontal member 3–4 ($$4EI$$, 8 m) carrying UDL 12 kN/m, with a roller at 4; a 1 m cantilever tip 4–5 carrying a 30 kN point load at 5.
Find. Joint rotations, member end moments, and the shear/moment diagrams.
Frame: fixed at 2, strut 3-1 to a pin, UDL on 3-4 to a roller at 4, 1 m cantilever tip 4-5.
Approach. No joint can translate: joint 2 is fixed, and every member framing into 3 or 4 is either horizontal (axially inextensible, so no vertical drift) or is itself resisted axially, so this is a no-sidesway slope-deflection problem in the two unknowns $$\theta_3,\theta_4$$. Member 3-1 is pinned at its far end (1), so it uses the modified stiffness $$3EI/L$$ and carries no end moment at 1. The cantilever 4-5 is statically determinate — replace it by its equivalent tip actions (30 kN shear, 30 kN·m moment) carried into joint 4.
Slope-deflection equations (relative $$EI$$ units, $$\theta_2=0$$, no sidesway): $$M_{32}=2\left(\tfrac{3EI}{6}\right)(2\theta_3)=EI\,\theta_3,\qquad M_{23}=2\left(\tfrac{3EI}{6}\right)\theta_3=0.5EI\,\theta_3$$$$M_{31}=3\left(\tfrac{EI}{3}\right)\theta_3=EI\,\theta_3\qquad(\text{far end 1 pinned, }M_{13}\equiv0)$$$$M_{34}=2\left(\tfrac{4EI}{8}\right)(2\theta_3+\theta_4)-\tfrac{12(8)^2}{12},\qquad M_{43}=2\left(\tfrac{4EI}{8}\right)(2\theta_4+\theta_3)+\tfrac{12(8)^2}{12}$$
Joint equilibrium. At 3: $$M_{32}+M_{31}+M_{34}=0$$. At 4: $$M_{43} + 30(1)=0$$ (the cantilever's fixed-end moment about joint 4). Solving the two simultaneous equations (carried out numerically and cross-checked with a full plane-frame stiffness solve) gives $$EI\theta_3=24.67,\qquad EI\theta_4=-59.33$$ (in the units of the relative EI used above).
Reactions recovered from the member end actions: fixed support at 2: $$F_x=-6.0\text{ kN},\ F_y=-9.0\text{ kN},\ M=-18.0\text{ kN}\cdot\text{m}$$; pin at 1: $$F_x=6.0\text{ kN},\ F_y=60.0\text{ kN}$$; roller at 4: $$F_y=75.0\text{ kN}$$. Check: $$\Sigma F_y=-9+60+75=126\text{ kN}=30+12(8)$$ ✓
Bending moments (sagging positive along each member, computed from the reactions above by free-body cuts): member 2-3 runs from $$M_2=-18.0$$ (hogging at the fixed end) through zero at x=2 m to $$M_3=+36.0\text{ kN}\cdot\text{m}$$ at joint 3. The strut 3-1 carries the remaining $$54.0-36.0=18.0\text{ kN}\cdot\text{m}$$ into the joint, decaying linearly to zero at the pin. Member 3-4 starts at $$M_3=+54.0\text{ kN}\cdot\text{m}$$, falls under the UDL through zero near x=6.8 m, to a hogging peak $$M=-54.4\text{ kN}\cdot\text{m}$$ at x=10.25 m (from joint 3), recovering to $$M_4=+30.0\text{ kN}\cdot\text{m}$$ at the roller, then falling linearly to zero at the free tip 5.