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)
42 kN at joint 3, along member 2–3 (direction 0.8, 0.6)
Components
\(F_x\) = 33.6 kN; \(F_y\) = 25.2 kN
Members
uniform EI, inextensible
Find. The member end moments, shears, axial forces and support reactions, and the bending moment diagram with its extreme ordinates.
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.
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.
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, \(\theta_2,\ \theta_3,\ \Delta\).
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):$$M_{12}=2k(\theta_2-3\psi),\quad M_{21}=2k(2\theta_2-3\psi),\quad M_{23}=2k(2\theta_2+\theta_3)$$$$M_{32}=2k(2\theta_3+\theta_2),\quad M_{34}=2k(2\theta_3-3\psi),\quad M_{43}=2k(\theta_3-3\psi)$$
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.
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.
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.
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.
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.
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: \(-168 + 72 + 96 = 0\).
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.