16-Civ-A1 Elementary Structural Analysis · December 2017
Question 7 of 8: Horizontal deflection by virtual work
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Exams, 16-Civ-A1 Elementary Structural Analysis, December 2017, 3 hours, closed book (approved Sharp or Casio calculator only). A complete paper is six questions: candidates answer all of Q1–Q5 and exactly one of Q6, Q7 or Q8. All eight questions are worked below — Q6, Q7 and Q8 each in full — so the set is a complete study resource. Marks: Q1 [6], Q2–Q5 [18 each], Q6–Q8 [22 each].
Reference texts: R.C. Hibbeler, Structural Analysis (10th ed., Pearson) — determinacy & stability (Ch. 2), method of joints/sections (Ch. 3), shear & moment diagrams (Ch. 4), deflections by virtual work (Ch. 8–9), influence lines (Ch. 6), slope–deflection and moment distribution (Ch. 11–12); A. Kassimali, Structural Analysis (6th ed., Cengage) — compound (Gerber) beams, internal hinges and condition equations, indeterminate frames. Sign convention: sagging bending moment positive (tension on the underside); truss forces tension (T) positive, compression (C) negative.
Reading the exam figures. Every support, member and load below was read directly from the printed figures. The Q4(b) truss carries a stray “3 m” label that is the perpendicular spacing between the two parallel chords (confirmed below), and the Q8 frame carries a stray “4.8 m” dimension that is not a load — it is the offset from the beam down to the lower dimension line (the columns are 4 m, stated on both outer columns).
Question 7 — Horizontal deflection by virtual work [22]
Portal: pin at 1, column 1–2 (10 m), beam 2–3 (20 m) with 20 kN at midspan, column 3–4 (10 m) to a roller at 4.
Given. A determinate portal (pin at 1, roller at 4). $20$ kN↓ at the beam midspan. $EI=2.0\times10^{5}$ kN·m² throughout.
Find. Horizontal deflection $\delta_{3h}$ at joint 3.
Approach. $\delta_{3h}=\displaystyle\int\frac{M\,m}{EI}\,ds$ with $M$ from the real load and $m$ from a unit horizontal load at 3. Both columns turn out to carry no product, so only the beam integral remains.
Real reactions. No horizontal load ⇒ $H_1=0$; $V_1=V_4=10$ kN. With $H_1=0$ both columns have zero real moment; the beam is a simple $20$ m span, $M_{\text{real}}$ a triangle peaking $-100$ kN·m at midspan (our sign: tension top).
Virtual system (unit → at 3). $H_1=-1$, $V_1=-0.5$, $V_4=+0.5$. Column 1–2 has $m=-y$ (0 to $-10$); the beam has $m=0.5x-10$ (from $-10$ at 2 to $0$ at 3); column 3–4 has $m=0$.
Only the beam contributes ($M_{\text{real}}=0$ in column 1–2; $m=0$ in column 3–4):$$\delta_{3h}=\frac{1}{EI}\int_0^{20} M_{\text{real}}(x)\,m(x)\,dx,\quad M_{\text{real}}=\begin{cases}-10x,&0\le x\le10\\10x-200,&10\le x\le20\end{cases},\ m=0.5x-10.$$
Evaluate. $\displaystyle\int_0^{20}M_{\text{real}}\,m\,dx=5000$ kN²·m³, so $$\delta_{3h}=\frac{5000}{2.0\times10^{5}}=0.025\text{ m}=\boxed{25\text{ mm}}.$$
Real bending moment on beam 2–3: simple-span triangle peaking $-100$ kN·m at midspan (columns carry zero real moment).
Quantity
Value
Real reactions
$H_1=0,\ V_1=V_4=10$ kN
$\int Mm\,dx$
$5000$ kN²·m³
Horizontal deflection at 3
$\delta_{3h}=25$ mm
Physical check. The $20$ kN sags the beam, rotating joints 2 and 3 outward; with only the pin restraining horizontal motion, joint 3 sways sideways. The $25$ mm result is confirmed by the finite-element model ($EA$ large so only flexure contributes).