16-Civ-B1 Advanced Structural Analysis · December 2017
Question 8 of 9: Symmetric frame with a Gerber top member (24 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examination, December 2017 — 16-Civ-B1 Advanced Structural Analysis. Three hours, closed book (an approved Sharp or Casio calculator is the only aid). Nine questions: both #1 and #2 are compulsory, then two only of #3, #4 or #5 and two only of #6, #7, #8 or #9 — six questions constitute a complete paper. Marks are printed in the left margin: 8, 12, 16, 16, 16, 24, 24, 24, 24. All nine questions are solved here, because the set is a study resource rather than a sitting.
Reference texts. R. C. Hibbeler, Structural Analysis, 10th ed. (Pearson) — Ch. 4 shear and moment diagrams, Ch. 9–10 the force (flexibility) method, Ch. 11 slope-deflection, Ch. 14–16 the stiffness method; A. Kassimali, Structural Analysis, 6th ed. (Cengage) — Ch. 7 deflections by work and energy (Castigliano and least work), Ch. 13 slope-deflection, Ch. 16 sidesway frames; W. McGuire, R. H. Gallagher and R. D. Ziemian, Matrix Structural Analysis, 2nd ed., for the planar frame element stiffness matrix used as the independent check on every answer below. Member sizing that would follow such an analysis is governed in Canada by CSA A23.3:19, CSA S16:19 and CSA O86:19, with load combinations from NBCC 2020.
Check: sign convention, stated once and used throughout. End moments $M_{ij}$ are counter-clockwise positive on the member end — the convention that matches the six-degree-of-freedom planar frame element, so every result below can be reproduced by a direct-stiffness solution. The chord rotation is $\psi_{ij}=\left[(\mathbf{D}_{j}-\mathbf{D}_{i})\cdot\mathbf{n}\right]/L$ with $\mathbf{n}$ the member axis turned $+90^\circ$; the fixed-end moment of a downward UDL is $\mathrm{FEM}_{ij}=+wL^{2}/12$ at the $i$ end; and the ordinary sagging moment is $M_{\text{sag}}(i)=-M_{ij}$, $M_{\text{sag}}(j)=+M_{ji}$. Mixing this with the clockwise-positive convention produces clean-looking integers that are wrong.
Question 8: Symmetric frame with a Gerber top member (24 marks)
Given. A symmetric frame of 22 m overall projection. Pins at joints 1 and 7 carry 3.75 m outer columns of stiffness $EI$; inclined members of stiffness $1.3EI$ rise 2.5 m over a 6 m run to joints 3 and 5 at 6.25 m; inner columns of stiffness $EI$ drop 5 m from joints 3 and 5 to fixed bases at joints 4 and 8, which sit 1.25 m above the outer supports. The 10 m top member (stiffness $1.3EI$) carries internal hinges 2 m in from each end. A UDL $w=30$ kN/m acts over the whole 22 m projection.
Question 8 — geometry, stiffness and loading
Member
Length
Relative $EI$
Notes
1–2 outer column
3.75 m
$EI$
pinned at joint 1
2–3 inclined
6.5 m (6 m run, 2.5 m rise)
$1.3EI$
carries the UDL over its 6 m projection
3–4 inner column
5.0 m
$EI$
fixed at joint 4
3–5 top member
10.0 m
$1.3EI$
hinges 2 m in from each end
5–6, 6–7, 5–8
mirror images of 2–3, 1–2 and 3–4
Loading
$w=30$ kN/m over the full 22 m projection, total 660 kN
Find. The end moments, and the shear force and bending moment diagrams with their maximum and minimum ordinates.
Q8: symmetric frame, pins at joints 1 and 7, fixed bases at joints 4 and 8, and internal hinges 2 m in from each end of the 10 m top member; w = 30 kN/m acts over the whole 22 m projection.
Approach. Strip the Gerber top member into a determinate suspended span plus two cantilevers, then use symmetry to show that the remaining half-frame cannot sway, leaving two rotations.
Take the suspended span first. The 6 m length between the two hinges has zero moment at both ends, so it is a simple span: $$R_{\text{hinge}}=\frac{30(6)}{2}=90\ \text{kN},\qquad M_{\text{mid}}=\frac{30(6)^{2}}{8}=\boxed{135\ \text{kN}\cdot\text{m}}$$
Turn each 2 m stub into a known joint action. The stub between joint 3 and the first hinge is a determinate cantilever carrying its own UDL plus the 90 kN handed over by the suspended span: $$M_{3,\text{beam}}=\frac{30(2)^{2}}{2}+90(2)=60+180=\boxed{240\ \text{kN}\cdot\text{m}},\qquad V_{3}=30(2)+90=150\ \text{kN}$$
Show the half-frame cannot sway. Every horizontal displacement in the chain 2–3–5–6 is the same because the top member and both inclined members are inextensible with vertical columns at their ends; symmetry requires $u_{5}=-u_{3}$, so both are zero. The inner column fixes $v_{3}=0$ and the outer column fixes $v_{2}=0$. Only $\theta_{2}$ and $\theta_{3}$ survive.
Write the fixed-end moment of the inclined member. The UDL is quoted per metre of horizontal projection, so the moment diagram along the member is the diagram of a horizontal beam of span 6 m; the flexibility integrals all pick up the same factor $L/L_{p}$, which cancels: $$\mathrm{FEM}_{23}=\frac{wL_{p}^{2}}{12}=\frac{30(6)^{2}}{12}=90\ \text{kN}\cdot\text{m}$$ The member stiffness, however, still uses the true length 6.5 m.
Write the two joint equations. With $k_{12}=3EI/3.75=0.8EI$ (pinned at joint 1), $k_{23}=2(1.3EI)/6.5=0.4EI$ and $k_{34}=2EI/5=0.4EI$, $$\text{joint 2:}\quad 1.6\,EI\theta_{2}+0.4\,EI\theta_{3}=-90$$ $$\text{joint 3:}\quad 0.4\,EI\theta_{2}+1.6\,EI\theta_{3}=90-240=-150$$
Recover the end moments. $$M_{21}=0.8(-35)=\boxed{-28.0},\qquad M_{23}=0.4(-155)+90=\boxed{+28.0}$$ $$M_{32}=0.4(-205)-90=\boxed{-172.0},\qquad M_{34}=0.8(-85)=\boxed{-68.0},\qquad M_{43}=0.4(-85)=\boxed{-34.0}$$ all in kN·m, with $M_{12}=0$ at the pin. Joint 3 balances: $-172-68+240=0$.
Find the peak sagging moment in the inclined member. Working on the equivalent 6 m horizontal span with end sagging moments $-28$ and $-172$, the end shear is $R=(540-172+28)/6=66$ kN, so the shear vanishes $2.2$ m along the projection: $$M_{\max}=-28+66(2.2)-15(2.2)^{2}=\boxed{+44.6\ \text{kN}\cdot\text{m}}$$
Two features of the answer are easy to mistake for errors. First, the bending moment steps at joint 3: the top member arrives with 240 kN·m while the inclined member leaves with 172 kN·m, and the 68 kN·m difference is exactly the moment driven into the inner column. Second, the load is shared very unevenly. The two inner columns take 260.9 kN each while the outer pins take only 69.1 kN each, because the stiff inner columns sit directly under the heavy end of the roof. The horizontal reactions are small and self-cancelling: 7.47 kN at each pin and 20.40 kN at each fixed base.
Q8: bending moment diagram on the tension side. The step at joint 3 (240 on the beam side against 172 on the rafter side) is the 68 kN.m carried into the inner column.
Question 8 — end actions and diagram ordinates
Member
Bending moment (kN·m)
Shear (kN)
1–2 outer column
0 at the pin, 28.0 at joint 2
7.47
2–3 inclined
28.0 hogging at joint 2, peak 44.6 sagging at 2.2 m along the projection, 172.0 hogging at joint 3
60.9 to 105.2 normal to the member
3–4 inner column
68.0 at joint 3, 34.0 at the fixed base (opposite faces)
20.4
3 to first hinge (2 m stub)
240.0 hogging at joint 3, zero at the hinge
150 falling to 90
Suspended span (6 m)
0 at each hinge, 135.0 sagging at mid-span
$\pm 90$
Right-hand half
mirror image of the left
Rotations
$EI\theta_{2}=-35$, $EI\theta_{3}=-85$ kN·m$^{2}$
Reactions
pins 1 and 7: 69.11 kN vertical with 7.47 kN horizontal; fixed bases 4 and 8: 260.89 kN vertical, 20.40 kN horizontal, 34.0 kN·m moment; total 660 kN