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04-BS-6 · December 2019

Question 2 of 8: Shear and Moment Diagrams for a Simply-Supported Beam

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

Notes on this paper

EGBC National Exam — Basic Studies, 04-BS-6 Mechanics of Materials, 2019-Dec. Closed book; one hand-written aid sheet permitted. The exam instructs "any FIVE of the eight questions constitute a complete paper," but every question is solved below as a full study resource.

Reference texts: Hibbeler, Mechanics of Materials, 10th ed. (axial deformation of composite members ch.4; shear/moment diagrams ch.6; stress transformation & Mohr's circle ch.9; buckling of columns ch.13; torsion of circular shafts ch.5; transformed-section composite beams ch.6; combined axial+bending+shear ch.8; beam deflection by integration ch.9). Standard W-shape table (exam Appendix C) is not needed by any question below.

Question 2: Shear and Moment Diagrams for a Simply-Supported Beam (20 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. Simply-supported steel beam, span $L=6\text{ m}$ (simple supports at $x=0$ and $x=6\text{ m}$ — the printed figure shows two support symbols, not a wall). UDL $w=3\text{ kN/m}$ over the last $2\text{ m}$ of the span ($4\le x\le6\text{ m}$). I-section: $d=220\text{ mm}$, $b_f=100\text{ mm}$, all thicknesses $=10\text{ mm}$ (used in Q3, not needed for $V,M$).

Find. $V(x)$, $M(x)$ over the full span, the diagrams, and the locations of maximum positive/negative moment and any inflection point.

3 kN/m 4 m 2 m
Simply-supported 6 m beam, UDL 3 kN/m over the last 2 m of the span.
Solved below as the simply-supported beam the figure actually shows.

Approach. Find the two reactions from statics on the whole span, then write $V(x)$ and $M(x)$ piecewise by direct integration of the load (no superposition), splitting at $x=4\text{ m}$ where the UDL begins.

  1. Reactions. UDL resultant $=3\times2=6\text{ kN}$ acting at its centroid $x=5\text{ m}$. $\sum M_{x=0}=0$: $R_6(6)-6(5)=0\Rightarrow R_6=5\text{ kN}$. $\sum F_y=0$: $R_0=6-5=\boxed{1\text{ kN}}$, $R_6=\boxed{5\text{ kN}}$.
  2. $V(x)$, $0\le x\le4$. No load in this stretch: $V(x)=R_0=1\text{ kN}$ (constant).
  3. $V(x)$, $4\le x\le6$. $V(x)=R_0-w(x-4)=1-3(x-4)\text{ kN}$; at $x=6^-$, $V=1-6=-5\text{ kN}=-R_6$, checks.
  4. $M(x)$, $0\le x\le4$. $M(x)=R_0\,x=x\text{ kN}\cdot\text{m}$ (linear, $M(4)=4\text{ kN}\cdot\text{m}$).
  5. $M(x)$, $4\le x\le6$. $M(x)=R_0x-\dfrac{w}{2}(x-4)^2=x-1.5(x-4)^2\text{ kN}\cdot\text{m}$; $M(6)=6-1.5(4)=0$, checks (simple support).
  6. Maximum moment. $V=0$ at $1-3(x-4)=0\Rightarrow x=4.333\text{ m}$: $M(4.333)=4.333-1.5(0.333)^2=\boxed{4.17\text{ kN}\cdot\text{m}}$ (positive/sagging). Since $V\ge0$ for $x\le4.333$ and $M(0)=M(6)=0$ at the two simple supports, $M(x)\ge0$ over the ENTIRE span — there is no negative-moment region and no inflection point for this support/load configuration.
Final results
QuantityValue
$R_0$ (left)1 kN
$R_6$ (right)5 kN
$M_{max}$ (at $x=4.333\text{ m}$)+4.17 kN·m (sagging)
Negative moment / inflection pointnone — $M(x)\ge0$ throughout