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07-Str-A4 · May 2018

Question 5 of 9: Uniform temperature rise in a three-column frame (16 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.

Reference texts.

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 5: Uniform temperature rise in a three-column 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 two-bay portal on three 6 m columns, unloaded, with every member lengthening by the same amount.

Given data — Question 5
ItemValue
columns 1–2, 6–3, 5–46.00 m each
beams 2–3 and 3–46.00 m each
support at joint 1pin
support at joint 6 (centre)fixed
support at joint 5pin
thermal elongation of every member0.006 m
flexural rigidityEI = 2.1 × 105 kN·m²
axial strain from stressneglected (members inextensible apart from the imposed elongation)

Find. Shear and bending moment diagrams with the maximum and minimum ordinate on every member.

2341656 m6 m6 mevery member lengthens 0.006 m; EI = 2.1 × 10⁵ kN·m²
Question 5: symmetric frame, pinned outer bases, fixed centre base, every member 6 m longer by 0.006 m.

Approach. The elongations prescribe every joint translation once symmetry fixes the centre joint, so the only unknown left is one joint rotation.

  1. Use symmetry to lock the centre joint. Geometry, supports and loading are all symmetric about the centre line through joints 3 and 6. A symmetric response has $u=0$ and $\theta=0$ on the axis of symmetry, so $$u_{3}=0,\qquad \theta_{3}=0,\qquad \theta_{4}=-\theta_{2}.$$
  2. Turn the elongations into joint displacements. Each column grows 0.006 m along its own axis, which is vertical, so every top joint rises: $v_{2}=v_{3}=v_{4}=+0.006$ m. Each beam grows 0.006 m horizontally, and with $u_{3}=0$ that spreads the frame symmetrically: $$u_{2}=-0.006\ \text{m},\qquad u_{4}=+0.006\ \text{m}.$$ Nothing else is free — the whole translation field is prescribed and no sway equation is needed.
  3. Compute the chord rotations. A chord rotation is the transverse relative displacement divided by the length. Both beams have $v_{2}=v_{3}=v_{4}$, so $\psi_{23}=\psi_{34}=0$; the centre column has $u_{3}=u_{6}=0$, so $\psi_{63}=0$; only the outer columns rotate, $$\psi_{12}=\frac{u_{2}-u_{1}}{6}=-0.001\ \text{rad},\qquad \psi_{54}=+0.001\ \text{rad}$$ (clockwise positive). This is the whole of the thermal loading.
  4. Write the slope-deflection equations. Joints 1 and 5 are pins, so use the modified form on the outer columns and the standard form on the beams: $$M_{21}=\frac{3EI}{6}\bigl(\theta_{2}-\psi_{12}\bigr),\qquad M_{23}=\frac{2EI}{6}\bigl(2\theta_{2}+\theta_{3}\bigr)=\frac{2EI}{3}\theta_{2}.$$ The centre column has $\theta_{3}=\theta_{6}=0$ and $\psi_{63}=0$, so $M_{36}=M_{63}=0$ before anything is solved — the centre column is completely unstressed.
  5. Solve the one joint equation. Moment equilibrium at joint 2 gives $$\frac{3EI}{6}\bigl(\theta_{2}+0.001\bigr)+\frac{2EI}{3}\theta_{2}=0\;\Rightarrow\;\theta_{2}\left(\frac{3}{6}+\frac{4}{6}\right)=-\frac{3(0.006)}{6^{2}},$$ that is $\tfrac{7}{6}\theta_{2}=-5.000\times10^{-4}$, so $$\boxed{\theta_{2}=-4.2857\times10^{-4}\ \text{rad}}$$ (clockwise positive; joint 4 rotates by the same amount the other way). Joint 3 is automatically in balance because $M_{32}$ and $M_{34}$ are equal and opposite by symmetry.
  6. Back-substitute for the end moments. With $EI=2.1\times10^{5}$ kN·m², $$M_{21}=\frac{3(2.1\times10^{5})}{6}\bigl(-4.2857\times10^{-4}+1.000\times10^{-3}\bigr)=\boxed{60.0\ \text{kN}\cdot\text{m}}$$ and the beam end moments follow as $M_{23}=-60.0$, $M_{32}=-30.0$ kN·m (magnitudes 60.0 and 30.0), with joint 2 in balance: $60.0-60.0=0$.
  7. Shears and reactions. Each outer column carries $$V=\frac{60.0}{6}=10.0\ \text{kN},$$ directed inwards at the base, so the pins push back with 10.0 kN horizontally (equal and opposite at joints 1 and 5, sum zero — the horizontal check). Each beam carries $$V=\frac{60.0+30.0}{6}=15.0\ \text{kN},$$ so the outer columns are in 15.0 kN compression and the centre column in 30.0 kN tension — a hold-down of 30.0 kN at joint 6, balanced by 15.0 kN of uplift resistance at each pin.
  8. Diagram shapes. No member carries a span load, so every shear diagram is a constant and every bending moment diagram is a straight line. The outer columns run from zero at the pin to 60.0 kN·m at the top; each beam runs from 60.0 kN·m hogging at its outer joint to 30.0 kN·m at the centre joint, with a point of contraflexure two-thirds of the way along; the centre column is a flat line at zero. Maximum ordinate 60.0 kN·m, minimum ordinate 0.
603060centre column: M = 0 everywherebending moments in kN·m (hogging plotted outside)
Question 5: bending moment diagram. The centre column carries nothing; every other end moment is 60.0 or 30.0 kN·m.
Question 5 — results
MemberBending moment (kN·m)Shear (kN)Axial (kN)
column 1–2 (and 5–4)0 at the pin, 60.0 at the top10.0 constant15.0 compression
centre column 6–30 throughout030.0 tension
beam 2–3 (and 3–4)60.0 at the outer joint, 30.0 at the centre joint15.0 constant10.0
joint rotation θ2−4.2857 × 10−4 rad——
horizontal reaction at each pin—10.0 (inward)—