16-Civ-B1 Advanced Structural Analysis · December 2017
Question 5 of 9: Slope-deflection for a frame jacked at joint 3 (16 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 5: Slope-deflection for a frame jacked at joint 3 (16 marks)
Given. A stepped frame of three 5 m members: a horizontal member 1–2 from a pin at joint 1, a vertical member 2–3 dropping to joint 3, and a horizontal member 3–4 running to a pin at joint 4. No applied loads; a jack raises joints 2 and 3 by 0.02 m.
Question 5 — data
Quantity
Value
Member 1–2, horizontal, pinned at 1
5 m
Member 2–3, vertical
5 m
Member 3–4, horizontal, pinned at 4
5 m
Imposed lift of joints 2 and 3
0.020 m upward
Flexural rigidity of every member
$EI=2.5\times10^{4}$ kN·m$^{2}$
Applied loads
none
Find. The end moments, the shear and bending moment diagrams with their extreme ordinates, and the force the jack must deliver.
Q5: pin at joint 1, horizontal member 1-2, vertical member 2-3, horizontal member 3-4, pin at joint 4; the jack under joint 3 raises joints 2 and 3 together.
Approach. The imposed lift is a prescribed displacement, so the chord rotations are known at the outset and the only unknowns are the two joint rotations, which anti-symmetry reduces to one.
Fix the kinematics. Member 1–2 is horizontal and inextensible from a pin, so $u_{2}=0$; member 3–4 likewise gives $u_{3}=0$; member 2–3 is vertical and inextensible, so $v_{2}=v_{3}$ — which is why lifting joint 3 necessarily lifts joint 2 by the same 0.020 m. There is no sway degree of freedom at all.
Write the chord rotations. With $\Delta=0.020$ m upward, $$\psi_{12}=-\frac{\Delta}{L}=-0.004,\qquad\psi_{23}=0,\qquad \psi_{34}=+\frac{\Delta}{L}=+0.004$$ the vertical member has no chord rotation because both its ends rise together.
Write the slope-deflection equations. Joints 1 and 4 are pins, so those members take the modified form: $$M_{21}=\frac{3EI}{L}\left(\theta_{2}-\psi_{12}\right),\qquad M_{34}=\frac{3EI}{L}\left(\theta_{3}-\psi_{34}\right)$$ $$M_{23}=\frac{2EI}{L}\left(2\theta_{2}+\theta_{3}\right),\qquad M_{32}=\frac{2EI}{L}\left(2\theta_{3}+\theta_{2}\right)$$
Use anti-symmetry and solve. Rotating the frame through $180^\circ$ about the mid-point of member 2–3 maps it onto itself and reverses the imposed lift, so $\theta_{3}=-\theta_{2}$. Joint 2 equilibrium $M_{21}+M_{23}=0$ then gives $$\left(\frac{3EI}{L}+\frac{2EI}{L}\right)\theta_{2}=-\frac{3EI\Delta}{L^{2}}\;\Longrightarrow\;\theta_{2}=-\frac{3\Delta}{5L}=-0.0024\ \text{rad}$$
Recover the end moments. With $EI/L=5000$ kN·m, $$M_{21}=3(5000)\left(-0.0024+0.004\right)=\boxed{24.0\ \text{kN}\cdot\text{m}}$$ and by anti-symmetry $M_{23}=-24.0$, $M_{32}=+24.0$, $M_{34}=-24.0$, with $M_{12}=M_{43}=0$ at the pins.
Get the shears and the jack force. Each horizontal member carries $$V=\frac{M_{21}}{L}=\frac{24}{5}=\boxed{4.8\ \text{kN}}$$ while the vertical member has $M_{23}+M_{32}=0$ and therefore zero shear and a constant moment of 24 kN·m. Both pins hold down with 4.8 kN, so the jack must push up with $\boxed{9.6\ \text{kN}}$.
The shape that falls out is unusually clean: the bending moment rises linearly from zero at each pin to 24 kN·m at the inner joint, and the column simply carries that 24 kN·m unchanged from top to bottom. Because the column takes no shear, it also takes no horizontal force, so both horizontal reactions are exactly zero — the entire jacking effort is resisted by a pair of 4.8 kN hold-down forces at the pins. That is the practical lesson of the question: jacking a member of a rigid frame does not just deflect it, it demands anchorage at supports that were never intended to carry uplift.
Q5: bending moment diagram drawn on the tension side. Both horizontal members run linearly from zero at the pin to 24 kN.m at the inner joint; the column carries a constant 24 kN.m and no shear.
Check: which joint the jack sits under. The printed text says “the jack under joint (2)” while the figure draws the jack under joint (3). The distinction does not change the analysis: member 2–3 is vertical and inextensible, so raising either joint raises both by the same amount, which is exactly what the sentence goes on to state. The 0.020 m lift of joints 2 and 3 is the datum used here.
Question 5 — end actions and diagram ordinates
Member
Bending moment
Shear
Axial
1–2 (horizontal)
0 at joint 1, 24.0 kN·m at joint 2
4.8 kN constant
0
2–3 (vertical)
24.0 kN·m constant
0
4.8 kN compression
3–4 (horizontal)
24.0 kN·m at joint 3, 0 at joint 4
4.8 kN constant
0
Joint rotations
$\theta_{2}=-2.4\times10^{-3}$ rad, $\theta_{3}=+2.4\times10^{-3}$ rad
Reactions
4.8 kN downward at each pin; horizontal reactions zero