Question 6 of 9: Slope-deflection with a uniformly distributed load and a support that moves outward (24 marks)
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examination, May 2018, 07-Str-A4 Advanced Structural Analysis — 3 hours, CLOSED BOOK (an approved Casio or Sharp calculator is permitted). Nine questions: #1 and #2 are compulsory (8 and 12 marks), then TWO of #3, #4, #5 (16 marks each) and TWO of #6, #7, #8, #9 (24 marks each); six questions constitute a complete paper (100 marks). All nine are solved here, because the set is a study resource rather than a timed sitting.
Ghali, A., Neville, A. M. and Brown, T. G., Structural Analysis: A Unified Classical and Matrix Approach, 7th ed., CRC Press — Ch. 4 (force method), Ch. 5 (displacement method), Ch. 24 (effects of temperature and lack of fit).
Canadian design context for the member sizing that follows this analysis: CSA S16:19 Design of Steel Structures, CSA A23.3:19 Design of Concrete Structures and the National Building Code of Canada 2020 (Part 4 loads and load combinations).
Sign convention used throughout. Member end moments $M_{ij}$ are counter-clockwise positive on the member end, which is the convention that matches the standard 6-degree-of-freedom element stiffness matrix and the counter-clockwise-positive joint rotations that Question 9 asks for. With that convention the fixed-end moment of a downward uniform load is $M^{F}_{ij}=+wL^{2}/12$ at the near end, the chord rotation is $\psi_{ij}=\left[(\mathbf{D}_{j}-\mathbf{D}_{i})\cdot\mathbf{e}_{2}\right]/L$ with $\mathbf{e}_{2}$ the member axis turned $+90^{\circ}$, and the ordinary sagging moments plotted on the diagrams are $M_{\text{sag}}(i)=-M_{ij}$ and $M_{\text{sag}}(j)=+M_{ji}$. Where a step of the working is quicker in the clockwise-positive (Hibbeler) form the sign is stated explicitly.
Question 6: Slope-deflection with a uniformly distributed load and a support that moves outward (24 marks)
Given. A two-member frame built in at joint 1 and pinned at joint 3, with the pin displaced horizontally outward.
Given data — Question 6
Item
Value
joint 1 (built in)
(0, 4) m
joint 2 (knee)
(8, 4) m
joint 3 (pin, displaced)
(11, 0) m
member 1–2
horizontal, 8.00 m, 1.2EI
member 2–3
inclined 3 m across and 4 m down, 5.00 m, EI
uniformly distributed load on 1–2
12 kN/m downward
outward movement of the pin at 3
16 mm
flexural rigidity
EI = 10 000 kN·m²
Find. Shear force and bending moment diagrams with the maximum and minimum ordinate on each member.
Question 6: the pin at joint 3 has been pushed 16 mm outward, which drags the knee at joint 2 downward.
Approach. Inextensibility of the two members turns the 16 mm support movement into a prescribed displacement of joint 2, leaving a single unknown rotation.
Fix the translations from inextensibility. Member 1–2 is horizontal and anchored at the built-in end, so $u_{2}=u_{1}=0$. Member 2–3 runs along $\mathbf{e}_{1}=(0.6,\,-0.8)$, and its length cannot change, so $$\bigl(\mathbf{D}_{3}-\mathbf{D}_{2}\bigr)\cdot\mathbf{e}_{1}=0\;\Rightarrow\;(0.016)(0.6)+(0-v_{2})(-0.8)=0,$$ giving $$\boxed{v_{2}=-0.012\ \text{m}}$$ The knee drops 12 mm. Both translations are now known, so the frame — which is two degrees statically indeterminate — is only one degree kinematically indeterminate.
Chord rotations. For the horizontal member the transverse displacement is the 12 mm drop over 8 m, $$\psi_{12}=+\frac{0.012}{8}=+1.500\times10^{-3}\ \text{rad (clockwise)}.$$ For the inclined member the transverse component of $\mathbf{D}_{3}-\mathbf{D}_{2}=(0.016,\,0.012)$ along $\mathbf{e}_{2}=(0.8,\,0.6)$ is $0.0200$ m over 5 m, so $$\psi_{23}=-4.000\times10^{-3}\ \text{rad (clockwise positive)}.$$
Fixed-end moments of the loaded member. The 12 kN/m load on the 8 m span gives, in the clockwise-positive form, $$M^{F}_{12}=-\frac{wL^{2}}{12}=-\frac{12(8)^{2}}{12}=-64.0\ \text{kN}\cdot\text{m},\qquad M^{F}_{21}=+64.0\ \text{kN}\cdot\text{m}.$$ Member 2–3 carries no span load.
Slope-deflection equations. With $2(1.2EI)/8=0.3EI$ on the beam and the modified $3EI/5=0.6EI$ on the member that is pinned at its far end, $$M_{12}=0.3EI\bigl(\theta_{2}-3\psi_{12}\bigr)-64,\qquad M_{21}=0.3EI\bigl(2\theta_{2}-3\psi_{12}\bigr)+64,$$ $$M_{23}=0.6EI\bigl(\theta_{2}-\psi_{23}\bigr),\qquad M_{32}=0 .$$
Joint 2 equilibrium gives the rotation. Setting $M_{21}+M_{23}=0$, $$1.2EI\,\theta_{2}+0.00105\,EI+64=0\;\Rightarrow\;\theta_{2}=-\frac{74.5}{1.2(10\,000)}=\boxed{-6.2083\times10^{-3}\ \text{rad}}$$ (clockwise positive, so the knee rotates counter-clockwise).
End moments. Substituting back, $$M_{12}=-96.13\ \text{kN}\cdot\text{m},\qquad M_{21}=+13.25\ \text{kN}\cdot\text{m},\qquad M_{23}=-13.25\ \text{kN}\cdot\text{m},\qquad M_{32}=0.$$ Joint 2 balances exactly, and as sagging ordinates the built-in end carries $$\boxed{M_{1}=-96.13\ \text{kN}\cdot\text{m (hogging)}}$$ while the knee carries $-13.25$ kN·m on both members.
Shears on the beam. With $M_{\text{sag}}$ known at both ends of the 8 m span, $$V_{1}=\frac{wL}{2}+\frac{M_{\text{sag}}(2)-M_{\text{sag}}(1)}{L}=48+\frac{-13.25+96.13}{8}=58.36\ \text{kN},$$ and $V_{2}=58.36-12(8)=-37.64$ kN. The shear passes through zero at $$x=\frac{58.36}{12}=4.863\ \text{m},$$ where the sagging moment peaks at $$\boxed{M_{\max}=+45.78\ \text{kN}\cdot\text{m}}$$ and the diagram crosses the axis at $x=2.10$ m and $x=7.62$ m.
The inclined member and the reactions. Member 2–3 carries no span load, so its moment falls linearly from 13.25 kN·m at the knee to zero at the pin, and its shear is constant, $$V_{23}=\frac{13.25}{5}=2.65\ \text{kN},$$ with an axial compression of 49.04 kN. Resolving that member force at joint 3 gives the reactions $$H_{1}=31.54\ \text{kN},\quad V_{1}=58.36\ \text{kN},\quad M_{1}=96.13\ \text{kN}\cdot\text{m};\qquad H_{3}=-31.54,\quad V_{3}=37.64\ \text{kN}.$$ The vertical reactions add to 96.0 kN, which is $12\times8$ — the load, exactly.
Question 6: shear force and bending moment diagrams for the loaded member 1–2; member 2–3 is linear between 13.25 kN·m and zero.
Question 6 — maximum and minimum ordinates
Member
Shear (kN)
Bending moment (kN·m, sagging +)
1–2 at joint 1 (built in)
+58.36
−96.13 (minimum)
1–2 at x = 4.863 m
0
+45.78 (maximum)
1–2 at joint 2
−37.64 (minimum)
−13.25
2–3 (constant shear)
+2.65
−13.25 at joint 2 to 0 at the pin
reactions
H = 31.54, V = 58.36 at joint 1; H = −31.54, V = 37.64 at joint 3