Question 2 of 9: Schematic shear force and bending moment diagrams
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.
R. C. Hibbeler, Structural Analysis, 10th ed. — Ch. 9 (deflections by energy methods), Ch. 10 (force/flexibility method), Ch. 11–12 (slope-deflection and moment distribution).
A. Kassimali, Structural Analysis, 6th ed. — Ch. 3 (determinacy and stability), Ch. 7 (deflections by work-energy), Ch. 16 (slope-deflection with sidesway).
A. Ghali, A. M. Neville and T. G. Brown, Structural Analysis: A Unified Classical and Matrix Approach, 7th ed. — Ch. 3–4 (force and displacement methods), Ch. 5 (lack of fit and support movement).
W. McGuire, R. H. Gallagher and R. D. Ziemian, Matrix Structural Analysis, 2nd ed. — Ch. 4–5 (member stiffness, assembly, kinematic constraints).
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
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 2: Schematic shear force and bending moment diagrams (12 marks)
Given. (a) A beam encastré at A, carried on rollers at B, C and D at spacings $L$, with two point loads $P$ at $L/3$ and $2L/3$ into span BC and a load $2P$ on a free overhang $L/3$ beyond D. (b) An L-shaped frame encastré at A, with a horizontal member AB of length $L$, a vertical member BC of length $L$ carrying a roller at its foot C, and a horizontal cantilever CD of length $L$ under a UDL $w$. All members share one $EI$ and are inextensible.
Find. The shape and the governing ordinates of the shear force and bending moment diagrams for both structures. Structure (a) is twice redundant and structure (b) once redundant, so the ordinates must come from an analysis, not from statics alone.
Structure (a): propped beam on three rollers with an overhang.
Approach. Both structures are analysed by the displacement method (equivalently three-moment or moment distribution for (a)); the determinate overhang and cantilever are replaced first by their statically equivalent end actions, which fixes one diagram ordinate before any analysis is done.
Fix the determinate ends of (a) by inspection. The overhang beyond D carries $2P$ at $L/3$, so
Solve the two redundancies. Taking the reactions at C and D as redundants (or equivalently writing three-moment equations for the interior supports) and using $EI$ constant gives the support reactions
Build the shear diagram of (a). Starting from $V=-0.3077P$ at A the shear is constant to B, jumps by $R_B$ to $+1.2564P$, steps down by $P$ at each point load, jumps by $R_C$ at C and by $R_D$ at D, and closes at $-2P$ at the free end.
Build the moment diagram of (a). The moment is piecewise linear because every load is a point load. The governing ordinates are $+0.103PL$ at the built-in end A, $-0.205PL$ over B, $+0.299PL$ under the second point load, $+0.051PL$ over C and $-0.667PL$ over D.
Reduce (b) to one unknown. Cantilever CD is determinate: at C it delivers a shear $wL$ and a hogging moment $wL^{2}/2$. Because the roller at C supplies no horizontal reaction and no horizontal load acts, the shear in column BC is identically zero, so BC carries a constant bending moment.
Solve (b). With that constant-moment column, the single compatibility condition gives $M_B=M_C=0.5wL^{2}$ hogging, a shear of $0.75wL$ in member AB and a sagging moment of $0.25wL^{2}$ at the built-in end A. Vertical equilibrium then returns $R_C=1.75wL$ upwards and a hold-down of $0.75wL$ at A.
whose sum is exactly the applied $4P$. Notice that the reaction at A is a hold-down: the heavy overhang load lifts the built-in end, which is why the fixed end carries a sagging moment of $+0.103PL$ rather than the hogging moment a candidate would expect.
Structure (a): shear force diagram (multiples of P).
Structure (a): bending moment diagram (sagging positive, multiples of PL).
Structure (b): L-frame with a roller foot and a loaded cantilever.
For structure (b) the cantilever fixes the diagram before any compatibility is written,
$$M_C=-\frac{wL^{2}}{2}=\boxed{-0.500\,wL^{2}}$$
and the remaining analysis distributes that moment back into the horizontal member, which finishes with $+0.25wL^{2}$ sagging at the encastré end A.
Structure (b): shear force developed along A-B-C-D.
Structure (b): bending moment developed along A-B-C-D.