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Question

For a simply supported beam with multiple point loads, maximum bending moment occurs where:

This question was previously asked in
RRB JE 2025 CBT 2 Mechanical and Allied Engg Question Paper English (2-Jul-2026) (Shift-1)
The correct answer is

Shear force = 0

This question relies on the fundamental differential relationships between load, shear force (V) and bending moment (M) along a beam. For a beam carrying a distributed load intensity w:

  • dV/dx = −w — the slope of the shear-force diagram equals the (negative of) the load intensity.
  • dM/dx = V — the slope of the bending-moment diagram equals the shear force at that section.

From calculus, the bending moment M reaches a maximum or minimum (a turning point) where its slope is zero, i.e. where dM/dx = 0. Because dM/dx = V, this condition becomes:

V = 0 → M is maximum (or minimum)

So the maximum bending moment occurs at the section where the shear force = 0, which on the shear-force diagram is exactly the point where the SFD crosses the zero (base) line. For a beam with several point loads, the SFD is a series of steps, and the critical section is the one at which the diagram changes sign.

The other conditions do not locate the maximum moment. Reaction = 0 would describe an unsupported point and has no general connection to where M peaks. Load = 0 is true along most of a beam that carries only point loads, so it cannot single out one section. Deflection = 0 occurs at the supports of a simply supported beam, but the maximum bending moment generally lies somewhere in the span, not at a support — so zero deflection does not mark the maximum moment. Hence the only correct criterion is shear force = 0.

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Similar Questions

  1. The maximum bending moment for a simply supported beam of span L with uniformly distributed load (UDL) w per unit length is _____.


Important Questions from Shear Force and Bending Moment

  1. A cantilever of length L carries a gradually (linearly) varying load from zero at its free end to w per unit length at the fixed end. The product of deflection and flexural rigidity at the free end is

  2. If the shear force at a section of a simply supported beam is zero, the bending moment at the section is

  3. Shear force at any point of the beam is the algebraic sum of

  4. A cantilever is subjected to a uniformly distributed load over its entire length. The variation of bending stress along the length of the cantilever is
  5. For a cantilever beam of length l carrying a concentrated load W at free end, the shear force and bending moment diagram will be

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