Question 6 of 8: Slope-Deflection Analysis of a Propped Frame
Nivaar worked solution (AI-drafted; not reviewed by a licensed engineer)
Notes on this paper
Paper format. National Examinations, December 2017, 07-Str-A1 Elementary Structural Analysis; three hours, closed book, approved Sharp or Casio calculator only. Six questions constitute a complete paper: Questions 1–5 are compulsory (6 + 18 + 18 + 18 + 18 = 78 marks) and the candidate answers one only of Questions 6, 7 or 8 (22 marks). All eight questions are worked below.
Sign conventions used throughout. Sagging bending moment is positive and is plotted above the axis; shear at a section is the sum of the upward forces on the portion to the left of it. Truss member forces are quoted as T for tension and C for compression. In the slope-deflection and moment-distribution work the member-end moments follow the usual convention — clockwise on the member end taken as positive — so the sagging moment is $+M_{ij}$ at the left end of a member and $-M_{ji}$ at its right end. Coordinates, where used, are measured from the left-hand support of the structure with $x$ to the right and $y$ upward.
Reference texts.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 2 (determinacy and stability), Ch. 3–5 (trusses, internal loadings, frames), Ch. 6 (influence lines), Ch. 8–9 (deflections; virtual work), Ch. 11–12 (slope deflection; moment distribution).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3 (equilibrium and determinacy), Ch. 4 (plane trusses), Ch. 5–6 (beams and frames), Ch. 7 (virtual work), Ch. 8–9 (influence lines), Ch. 16–17 (slope deflection; moment distribution).
K. Leet, C.-M. Uang and A. Gilbert, Fundamentals of Structural Analysis, 5th ed. — a parallel treatment of the same syllabus.
C. H. Norris, J. B. Wilbur and S. Utku, Elementary Structural Analysis, 4th ed. — the classical text this exam code is named after.
Question 6: Slope-Deflection Analysis of a Propped Frame (22 marks)
12 kN/m over the whole 8 m of ③–④; 30 kN down at the tip ⑤
Find. The end moments by slope deflection, the reactions, and the shear force and bending moment diagrams of every member with maximum and minimum ordinates labelled.
Question 6 — the frame; node ② is built into the wall, ④ is a roller and the column foot ① is a pin.
Approach. Show first that the frame cannot sway, so the only unknowns are the joint rotations at ③ and ④; write the slope-deflection equations with the modified stiffness $3EI/L$ for the pin-based column, take the overhang moment into joint ④ as a known applied moment, and solve two simultaneous equations.
Establish that there is no sidesway. Node ② is built in, and member ②–③ is inextensible, so ③ cannot move horizontally; member ③–④ then fixes ④ horizontally as well. Vertically, the inextensible column pinned at ① holds ③ and the roller holds ④. Every joint translation is therefore prevented and the chord rotations $\psi$ are all zero — which is exactly what the phrase “members are inextensible” in the question is there to license. The unknowns are the two rotations $\theta_3$ and $\theta_4$.
Fixed-end moments and member stiffnesses. Only span ③–④ is loaded, giving $\mathrm{FEM}_{34} = -wL^2/12 = -12(8)^2/12 = -64$ kN.m and $\mathrm{FEM}_{43} = +64$ kN.m. The stiffness coefficients are $2E(3I)/6 = EI$ for the 6 m beam and $2E(4I)/8 = EI$ for the 8 m beam, so both spans happen to share the same coefficient. The column is pinned at ①, so use the modified form $M_{31} = (3EI/L)\theta_3 = EI\theta_3$ with $M_{13} = 0$ and no carry-over.
Write the slope-deflection equations. With $\theta_2 = 0$ at the built-in end, $$M_{23} = EI\theta_3, \qquad M_{32} = 2EI\theta_3$$ $$M_{34} = EI(2\theta_3 + \theta_4) - 64, \qquad M_{43} = EI(2\theta_4 + \theta_3) + 64$$ and $M_{31} = EI\theta_3$ for the column.
The overhang delivers a known moment to joint ④. The 1 m tip carries 30 kN, so the sagging moment at ④ taken from the right is $-30(1) = -30$ kN.m. Since ④ is the left end of member ④–⑤, that sagging value is $M_{45}$, so joint equilibrium reads $M_{43} + M_{45} = 0$, that is $M_{43} = +30$ kN.m. The overhang has no stiffness and must never be given a share of any balancing moment; it enters only through this fixed value.
Solve the two joint equations. Joint ③ requires $M_{32} + M_{34} + M_{31} = 0$, which gives $EI(5\theta_3 + \theta_4) = 64$; joint ④ requires $M_{43} = 30$, which gives $EI(\theta_3 + 2\theta_4) = -34$. Solving, $$EI\theta_3 = 18, \qquad EI\theta_4 = -26$$ Exact integers, which is the confirmation that the sign of the overhang moment was taken correctly — the opposite sign gives ragged decimals and nothing else in the solution lands on a round number.
Back-substitute for the end moments. $$\boxed{M_{23} = +18,\quad M_{32} = +36,\quad M_{34} = -54,\quad M_{43} = +30,\quad M_{31} = +18\ \text{kN.m}}$$ Joint ③ checks at once: $36 - 54 + 18 = 0$.
Member shears and reactions. Span ②–③ carries no load, so its shear is constant at $(-36 - 18)/6 = -9$ kN. On span ③–④, writing $M(x) = -54 + V_3x - 6x^2$ and forcing $M(8) = -30$ gives $V_3 = +51$ kN, falling to $-45$ kN at ④. The overhang carries a constant $+30$ kN. The column moment runs from $+18$ kN.m at ③ to zero at the pin over 3 m, so its shear is 6 kN. The reactions follow: at the built-in end ②, $9$ kN downward together with $6$ kN horizontal and a fixing moment of $18$ kN.m; at the column pin ①, $60$ kN upward and $6$ kN horizontal the other way; at the roller ④, $75$ kN upward. Vertical equilibrium closes: $-9 + 60 + 75 = 126 = 12(8) + 30$ kN.
Extreme ordinates for the diagrams. The shear is $-9$ kN throughout ②–③, rises to $+51$ kN at ③ and crosses zero $51/12 = 4.25$ m along the loaded span before reaching $-45$ kN at the roller. The peak sagging moment there is $$M_{\max} = -54 + \frac{51^2}{2(12)} = \boxed{+54.375\ \text{kN.m}}$$ The beam moment is $+18$ kN.m at the wall, falls through zero at 1.33 m, reaches $-36$ kN.m just left of ③ and jumps to $-54$ kN.m just right of it — the jump being exactly the 18 kN.m the column delivers — then swings positive over most of the loaded span and closes at $-30$ kN.m over the roller before running out to zero at the tip.
Question 6 — shear force and bending moment diagrams.