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)
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.
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.
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.