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16-Civ-B1 Advanced Structural Analysis · May 2014

Question 5 of 9: Slope-deflection analysis of a propped gable frame

Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)

Notes on this paper

Paper format. National Examination, May 2014, 98-Civ-B1 Advanced Structural Analysis — 3 hours, closed book (approved Sharp or Casio calculator permitted). Nine questions over seven pages: Questions 1 and 2 are compulsory (8 and 12 marks), then any two of Questions 3, 4, 5 (16 marks each) and any two of Questions 6, 7, 8, 9 (24 marks each). Six questions constitute a complete paper and total 100 marks. Marks are printed in the left margin. All nine questions are solved here, because the set is a study resource rather than a three-hour sitting.

Reference texts.

Throughout this paper end moments are quoted with the counter-clockwise-positive sign convention, the one that matches the standard six-degree-of-freedom stiffness element. In that convention the slope-deflection equation is

$$M_{ij}=\frac{2EI}{L}\bigl(2\theta_i+\theta_j-3\psi_{ij}\bigr)+\mathrm{FEM}_{ij}$$

the chord rotation is $\psi_{ij}=\bigl[(\mathbf{d}_j-\mathbf{d}_i)\cdot\mathbf{e}_2\bigr]/L$ with $\mathbf{e}_2$ the member axis turned $+90^\circ$, the fixed-end moment of a downward UDL is $\mathrm{FEM}_{i}=+wL^{2}/12$ and $\mathrm{FEM}_{j}=-wL^{2}/12$, and the ordinary sagging bending moment is recovered as $M_{\text{sag}}(i)=-M_{ij}$, $M_{\text{sag}}(j)=+M_{ji}$. Mixing this with the clockwise-positive convention of some textbooks is the single most common source of clean-looking but wrong answers on this paper.

Question 5: Slope-deflection analysis of a propped gable frame (16 marks)

Question text not reproduced: the examination questions are © Engineers and Geoscientists BC. Open the official past paper (linked at the top of this page) to read the question, then follow the worked solution below.

Given. A symmetric-looking gable frame with equal rafters, propped at its apex by a fixed-base column, with short free stubs beyond each springing and a UDL over the right-hand half.

Given data
ItemValue
Stub ①–② and ④–⑤2 m each (free ends at ① and ⑤)
Rafter horizontal projection ②–③ and ③–④6 m each
Apex rise above the springing level2.5 m
Rafter length$\sqrt{6^{2}+2.5^{2}}=6.5$ m
Apex ③ to the fixed base ⑥6.5 m (4.0 m below the springing level)
Support at ②roller (vertical only)
Support at ④pin
Support at ⑥encastré
UDL from ③ to ⑤20 kN/m on the horizontal projection (8 m)
Flexural rigiditythe same $EI$ in every member

Find. All member end moments, hence the shear force and bending moment diagrams with their maximum and minimum ordinates.

20 kN/m1234562 m6 m6 m2 m2.5 m6.5 m
Question 5: propped gable frame, UDL specified per metre of horizontal projection.

Approach. Prove first that inextensibility forbids sway, so the analysis carries only joint rotations; replace the two free stubs by their statically equivalent joint actions; then write slope-deflection equations for the rafters and the column and solve the two independent joint-moment equations.

  1. Kill the sway before writing anything. The column ③–⑥ is vertical and inextensible with a fixed base, so $v_3=0$; the pin at ④ gives $u_4=v_4=0$; the inextensible rafter ③–④ then forces $\mathbf{d}_3\cdot\mathbf{e}_{34}=0$, i.e. $u_3=0$. Joint ③ is therefore fully restrained in translation and, working back along rafter ②–③, so is ②. Every chord rotation vanishes.
  2. Deal with the two free stubs. Stub ①–② carries nothing, so member ①–② is a zero-force member and $M_{21}=0$, which forces $M_{23}=0$ and lets the rafter be handled with the modified stiffness $3EI/L$. Stub ④–⑤ is a 2 m cantilever under the UDL and applies a known hogging moment $20(2)(1)=40$ kN·m and a shear of 40 kN to joint ④.
  3. Get the fixed-end moments of the loaded rafter. A UDL specified per metre of horizontal projection on an inclined member has fixed-end moments $w\,L_{\text{proj}}^{2}/12$ — the projection, not the sloping length — because the transverse component is $w\cos^{2}\alpha$ and $L\cos\alpha=L_{\text{proj}}$.
  4. Write the slope-deflection equations. With $k=EI/6.5$ and all $\psi=0$: $M_{32}=3k\theta_3$ (modified stiffness), $M_{36}=4k\theta_3$, $M_{63}=2k\theta_3$, $M_{34}=2k(2\theta_3+\theta_4)+60$ and $M_{43}=2k(2\theta_4+\theta_3)-60$.
  5. Impose joint equilibrium. At ③, $M_{32}+M_{34}+M_{36}=0$ gives $11k\theta_3+2k\theta_4=-60$; at ④, the cantilever fixes $M_{43}=-40$ and gives $2k\theta_3+4k\theta_4=20$.
  6. Solve and back-substitute. The two-by-two system returns $k\theta_3=-7.0$ and $k\theta_4=+8.5$ kN·m, whence all five end moments follow directly and the joint check $-21+49-28=0$ closes exactly.

The fixed-end moment of the loaded rafter is

$$\mathrm{FEM}_{34}=\frac{w\,L_{\text{proj}}^{2}}{12}=\frac{20(6)^{2}}{12}=+60\text{ kN}\cdot\text{m},\qquad \mathrm{FEM}_{43}=-60\text{ kN}\cdot\text{m}$$

and solving the two joint equations gives the end moments

$$\boxed{M_{32}=-21.0,\quad M_{34}=+49.0,\quad M_{36}=-28.0,\quad M_{43}=-40.0,\quad M_{63}=-14.0\ \text{kN}\cdot\text{m}}$$

Converted to ordinary sagging moments, rafter ②–③ runs from zero at the roller to $-21.0$ kN·m at the apex, while rafter ③–④ starts at $-49.0$ kN·m on the other side of the same joint. The 28.0 kN·m step between them is the column moment, and that step is joint equilibrium rather than an error. Between the two ends the rafter carries the free parabola of the projected UDL, peaking at $+45.6$ kN·m at $x=11.08$ m.

Bending moment along 2-3-4-5 (sagging +ve)kN·m-21.0 (rafter 2-3)-49.0 (rafter 3-4)+45.6-40.02345
Question 5: bending moment developed along ②-③-④-⑤, sagging positive.

The reactions follow from member equilibrium and confirm the analysis: $R_2=-3.50$ kN (a hold-down at the roller), $V_4=101.2$ kN, $H_4=-6.46$ kN, and at the column base $V_6=62.3$ kN, $H_6=+6.46$ kN with $M_6=-14.0$ kN·m. Vertical equilibrium closes on the applied $20(8)=160$ kN and the two horizontal reactions cancel, as they must under purely vertical loading.

MemberEnd moment (CCW +ve)Comment
②–③$M_{23}=0$, $M_{32}=-21.0$moment-free at the roller (stub carries nothing)
③–④$M_{34}=+49.0$, $M_{43}=-40.0$loaded rafter; max sagging $+45.6$ at $x=11.08$ m
③–⑥ (column)$M_{36}=-28.0$, $M_{63}=-14.0$shear $6.46$ kN, axial $62.3$ kN
④–⑤ (stub)$M_{45}=+40.0$, $M_{54}=0$determinate cantilever, shear 40 kN
Reactions$R_2=-3.50$, $V_4=101.2$, $V_6=62.3$ kN$\sum V=160$ kN = $20(8)$