24-Bld-A1 Elementary Structural Analysis · December 2016
Question 2 of 8: Reactions, shear and bending-moment diagrams for three determinate structures (18 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
National Exams, December 2016 — 07-Bldg-A1 Elementary Structural Analysis. 3 hours. Six questions constitute a complete paper: answer ALL of Questions #1–#5; answer ONLY ONE of #6, #7 or #8 (all three are solved below for completeness).
Given. Pin at A ($x=0$), roller at B ($x=12\text{ m}$), free tip C ($x=16\text{ m}$); a 60 kN point load at $x=6\text{ m}$ and a 6 kN/m UDL from $x=6\text{ m}$ to the tip.
Find. $R_A$, $R_B$, and the shear/moment diagrams with every segment's max/min ordinate.
Fig. Q2(a) — beam with 4 m overhang past roller B.
Approach. Two global equilibrium equations solve the two unknown reactions; shear and moment then follow segment by segment from the left.
Bending moment diagram. $M(6)=35(6)=\boxed{+210\text{ kN}\cdot\text{m}}$ (peak sagging, under the point load). $M(12)=210+(-25)(6)-3(6)^2=\boxed{-48\text{ kN}\cdot\text{m}}$ (hogging, over support B). $M(16)=-48+24(4)-3(4)^2=0$, confirming the free tip.
Q2(a) – reactions and diagram extremes
Quantity
Value
$R_A$
35 kN ↑
$R_B$
85 kN ↑
$V_{\max}$ (span AB)
+35 kN (0–6 m)
$V_{\min}$ (span AB)
−61 kN (at B−)
$V_{\max}$ (overhang BC)
+24 kN (at B+)
$M_{\max}$ (sagging)
+210 kN·m at $x=6$ m
$M_{\min}$ (hogging)
−48 kN·m at B
(b) Propped cantilever with an internal hinge
Given. Fixed at A ($x=0$), internal hinge H at $x=4\text{ m}$, roller at $x=10\text{ m}$, free tip at $x=14\text{ m}$; UDL 6 kN/m over the full 14 m.
Find. $R_A$, $M_A$, and shear/moment diagrams for both spans.
Fig. Q2(b) — cantilever A–H carrying a suspended span H–roller–tip.
Approach. Split at the hinge (zero moment, shear-only transfer): solve the right sub-beam H–roller–tip on its own, then apply the hinge's reaction as a downward point load on the left cantilever A–H.
Right sub-beam (H to tip, 10 m, own UDL 60 kN, centroid at 5 m). $\sum M_H=0$: $R_{\text{roller}}(6)=60(5) \Rightarrow R_{\text{roller}}=50\text{ kN}$. $\sum F_y=0$: $R_H=60-50=\boxed{10\text{ kN}}$ — this is the downward force the hinge transmits onto the left cantilever's tip.
Left cantilever (A to H, 4 m, own UDL 24 kN plus the 10 kN hinge load at the tip). $R_A=24+10=\boxed{34\text{ kN}}$. $M_A=24(2)+10(4)=48+40=\boxed{88\text{ kN}\cdot\text{m}}$ (hogging).
Shear/moment by segment. A–H: $V$ falls linearly $34\to10$ kN; $M$ rises monotonically $-88\to0$ kN·m (zero at the hinge, as required). H–roller: $V$ falls $10\to-26$ kN, crossing zero at $x=4+1.67=5.67\text{ m}$ where $M=\boxed{+8.33\text{ kN}\cdot\text{m}}$ (local sagging peak); $M$ reaches $-48$ kN·m at the roller. Roller–tip: $V$ falls $24\to0$ kN; $M$ rises $-48\to0$ kN·m at the free tip.
Given. Pin at A $(0,0)$, rafter to a rigid peak at $(12,9)$, rafter down to a roller at D $(15,5)$ (D sits 5 m above A). UDL 10 kN/m on the horizontal projection, full 15 m.
Find. $R_A$, $R_D$, and the shear/moment diagram along each rafter.
Fig. Q2(c) — asymmetric gable frame; UDL is per horizontal metre.
Approach. Resolve the horizontal-projection UDL into an equivalent load per metre of each inclined rafter ($w_{\text{eff}}=w\cos\theta$), then take global equilibrium (only vertical reactions arise since the total load is vertical and there is no other horizontal action) followed by a section cut along each rafter for shear and moment.
Equivalent rafter loads. Rafter A–Peak: length $15\text{ m}$ (9,12,15 triple), horizontal run 12 m $\Rightarrow$ total load $=10(12)=120\text{ kN}$, centroid at $x=6$. Rafter Peak–D: length 5 m, horizontal run 3 m $\Rightarrow$ total load $=10(3)=30\text{ kN}$, centroid at $x=13.5$.
Reactions. Total $W=150\text{ kN}$ at $\bar x=\dfrac{120(6)+30(13.5)}{150}=7.5\text{ m}$. $\sum M_A=0$: $R_D(15)=150(7.5)\Rightarrow R_D=\boxed{75\text{ kN}}$. $\sum F_y=0$: $R_A=\boxed{75\text{ kN}}$ (both vertical; $R_{Ax}=0$ since the load has no horizontal component and only one support resists horizontal thrust—confirmed by the frame solve).
Rafter A–Peak (local $x$ from A, $w_{\text{trans}}=8\times12/15=6.4\text{ kN/m}$ transverse component). $V(0)=+60\text{ kN}$, falling to $V(15)=-36\text{ kN}$ at the peak, crossing zero at $x=9.375\text{ m}$ where $M=\boxed{+281.25\text{ kN}\cdot\text{m}}$ — the governing design moment for the whole frame. $M(\text{peak})=+180\text{ kN}\cdot\text{m}$.
Rafter Peak–D. $V$ runs $-27\to-45\text{ kN}$ (one sign throughout, so no interior extremum): $M$ falls monotonically from $+180$ kN·m at the peak to $0$ at the roller D.