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07-Str-A4 · May 2016

Question 7 of 8: Frame with an Inclined Member and Two Built-in Bases at Different Levels

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

Notes on this paper

Paper format. National Examinations, May 2016 — 07-Str-A4 Advanced Structural Analysis, three hours, closed book (an approved Sharp or Casio calculator is permitted). Questions 1 and 2 are compulsory at 8 marks each; the candidate then answers two of Questions 3, 4 or 5 and two of Questions 6, 7 or 8 at 21 marks each, so six questions make a complete paper of 100 marks. All eight questions are worked here, because this set is a study resource rather than a sat examination.

Reference texts. R. C. Hibbeler, Structural Analysis, 10th ed. (Ch. 6 influence lines, Ch. 9 virtual work and Castigliano, Ch. 10 force method, Ch. 11 slope-deflection, Ch. 12 moment distribution, Ch. 16 stiffness method for frames); A. Kassimali, Structural Analysis, 6th ed.; A. Ghali, A. M. Neville & T. G. Brown, Structural Analysis: A Unified Classical and Matrix Approach, 7th ed.; J. C. McCormac, Structural Analysis: Using Classical and Matrix Methods, 4th ed. Canadian design context for the same structures: CSA S16, CSA A23.3 and the National Building Code of Canada 2020.

Check: sign conventions used throughout. Slope-deflection and moment-distribution end moments \(M_{ij}\) and joint rotations \(\theta\) are clockwise positive (Hibbeler), and the chord rotation \(\psi_{ij}\) is positive when the member chord rotates clockwise. Internal bending moments are plotted sagging positive, converted from the end moments by \(M_{\text{sag}}(i)=M_{ij}\) at the near end and \(M_{\text{sag}}(j)=-M_{ji}\) at the far end. Truss bar forces are tension positive.

Question 7: Frame with an Inclined Member and Two Built-in Bases at Different Levels (21 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.

ItemValue
Joint coordinates1 (0, 0); 2 (0, 5); 3 (4, 8); 4 (4, 3) m
Member lengths1–2 = 5 m; 2–3 = 5 m (4–3–5 triangle); 3–4 = 5 m
Supportsjoints 1 and 4 fully built in
Load42 kN at joint 3, along member 2–3 (direction 0.8, 0.6)
Components\(F_x\) = 33.6 kN; \(F_y\) = 25.2 kN
Membersuniform EI, inextensible

Find. The member end moments, shears, axial forces and support reactions, and the bending moment diagram with its extreme ordinates.

42 kN12345 m3 m5 m3 m4 m
Question 7 — both column bases are fully built in and the two bases are at different levels; the 42 kN load acts at joint 3 along the axis of member 2–3. All members inextensible with the same EI.

Approach. Prove that the sway pattern has a single parameter, write the three slope-deflection equations, close the system with the virtual-work sway equation for a unit horizontal translation, and finish with statics. All three members happen to be 5 m long, which makes the algebra unusually clean.

  1. Resolve the load. Member 2–3 has a 4 m run and a 3 m rise, so its unit vector is \((0.8,\,0.6)\) and$$F_x = 42(0.8) = 33.6\ \text{kN},\qquad F_y = 42(0.6) = 25.2\ \text{kN}$$both positive, i.e. up and to the right.
  2. Establish the sway pattern from inextensibility alone. Both columns are vertical and inextensible, so \(v_2 = v_1 = 0\) and \(v_3 = v_4 = 0\). The inclined member is then inextensible only if$$(u_3-u_2)(0.8) + (v_3-v_2)(0.6) = 0 \;\Longrightarrow\; u_3 = u_2 = \Delta$$so both joints translate horizontally by the same amount and the inclined member has zero chord rotation:$$\psi_{12} = \psi_{34} = \frac{\Delta}{5},\qquad \psi_{23} = 0$$That single observation removes the usual difficulty with inclined members and leaves three unknowns, \(\theta_2,\ \theta_3,\ \Delta\).
  3. Slope-deflection equations. With \(k = EI/5\) for every member, \(\theta_1 = \theta_4 = 0\), and no span loads (the 42 kN acts at a joint):$$M_{12}=2k(\theta_2-3\psi),\quad M_{21}=2k(2\theta_2-3\psi),\quad M_{23}=2k(2\theta_2+\theta_3)$$$$M_{32}=2k(2\theta_3+\theta_2),\quad M_{34}=2k(2\theta_3-3\psi),\quad M_{43}=2k(\theta_3-3\psi)$$
  4. Joint equilibrium. Balancing joints 2 and 3,$$4\theta_2 + \theta_3 - 3\psi = 0,\qquad 4\theta_3 + \theta_2 - 3\psi = 0$$Subtracting shows \(\theta_2 = \theta_3 = \theta\), whence \(5\theta = 3\psi\), i.e. \(\theta = 0.6\psi\). The equality of the two joint rotations is a consequence of the equal member lengths and of the load acting only at a joint.
  5. Sway equation by virtual work. Give the frame a virtual translation \(\Delta^{*} = 1\) to the right; the two columns take \(\psi^{*} = 1/5\), the inclined member takes \(\psi^{*} = 0\), and joint 3 moves one unit horizontally so the applied load does work \(F_x\). Then$$\frac{M_{12}+M_{21}}{5} + \frac{M_{34}+M_{43}}{5} + F_x = 0$$$$\Longrightarrow\; 4k\left(3\theta - 6\psi\right) = -5(33.6) \;\Longrightarrow\; k\psi = \boxed{10.0},\quad k\theta = 6.0$$so \(EI\theta = 30.0\) and \(EI\Delta = 5EI\psi = 250\), a sway to the right of \(250/EI\) metres — the same sense as the horizontal component of the load, as it must be.
  6. Member end moments. Substituting \(k\theta = 6.0\) and \(k\psi = 10.0\),$$M_{12} = 2(6-30) = -48.0,\qquad M_{21} = 2(12-30) = -36.0$$$$M_{23} = M_{32} = 2(3\times 6) = +36.0,\qquad M_{34} = -36.0,\qquad M_{43} = -48.0\ \text{kN}\cdot\text{m}$$Both joints balance to zero. In the sagging convention the base moments are$$\boxed{M_1 = M_4 = 48.0\ \text{kN}\cdot\text{m}},\qquad \boxed{M_2 = M_3 = 36.0\ \text{kN}\cdot\text{m}}$$the frame being point-symmetric in its response even though its geometry is not mirror-symmetric.
  7. 48363648
    Question 7 — bending moment diagram drawn normal to each member (ordinates in kN·m). Every member has a straight moment line because none carries a span load; the contraflexure point in each column is where the diagram crosses the axis.
  8. Shears and the storey check. With no span load each member has a constant transverse shear:$$V_{1\text{-}2} = \frac{48.0+36.0}{5} = 16.8\ \text{kN},\qquad V_{3\text{-}4} = \frac{48.0+36.0}{5} = 16.8\ \text{kN}$$$$V_{2\text{-}3} = \frac{36.0+36.0}{5} = 14.4\ \text{kN}$$The two column shears sum to \(33.6\) kN, exactly the applied horizontal component — the decisive arithmetic check on the sway equation.
  9. Axial forces and reactions. Global equilibrium, using the two base fixing moments of 48.0 kN·m, gives$$H_1 = H_4 = -16.8\ \text{kN},\qquad V_1 = -30.6\ \text{kN},\qquad V_4 = +5.4\ \text{kN}$$so the left base is a hold-down of 30.6 kN. Resolving at the joints, member 1–2 carries 30.6 kN tension, member 2–3 carries 31.8 kN tension and member 3–4 carries 5.4 kN compression. Moments about joint 4 close the check: \(-168 + 72 + 96 = 0\).
  10. Reading the diagrams. Every member has a straight moment line, so each has exactly one point of contraflexure. In column 1–2 it lies \(48.0/(48.0+36.0) \times 5 = 2.857\) m above the base; in the inclined member it is exactly at mid-length, because the two end moments are equal in magnitude and opposite in sagging sense; in column 3–4 it lies 2.857 m above joint 4. The largest moment anywhere in the frame is 48.0 kN·m at each built-in base.
QuantityValue
Load components33.6 kN horizontal, 25.2 kN vertical (up)
Joint rotations\(EI\theta_2 = EI\theta_3 = 30.0\) (clockwise positive)
Sway\(\Delta = 250/EI\) to the right
Base moments \(M_1,\ M_4\)48.0 kN·m each (maximum ordinates)
Joint moments \(M_2,\ M_3\)36.0 kN·m each
Member shears16.8 / 14.4 / 16.8 kN in members 1–2, 2–3, 3–4
Axial forces30.6 kN T, 31.8 kN T, 5.4 kN C
Reactions\(H_1 = H_4 = 16.8\) kN (leftward); \(V_1 = 30.6\) kN down; \(V_4 = 5.4\) kN up
Points of contraflexure2.857 m from each base; mid-length of member 2–3