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A simply supported beam of span l, carrying point load W at centre of span, slope at both end will be
24EIWl3
48EIWl3
16EIWl2
384EI5wl4
16EIWl2
For a simply supported beam of span l subjected to a central point load W, the slope θ at both supports is equal to 16EIWl2. This is derived from the standard elastic curve equation for structural members under static loading.
For a simply supported beam of span l subjected to a central point load W, the slope θ at both supports is equal to 16EIWl2. This is derived from the standard elastic curve equation for structural members under static loading.
θ=16EIWl2 — Slope at supports
δmax=48EIWl3 — Maximum deflection at center
When a point load acts at the center of a simply supported beam, the beam undergoes bending, resulting in a maximum deflection at the center and maximum slope at the supports. Using the double integration method or Macaulay's method, the slope equation is θ=kcdotEIM⋅L, where the specific distribution of the bending moment for a central load results in the factor of 16 at the supports.
Slope is maximum at the ends (supports) and zero at the center.
Deflection is maximum at the center and zero at the supports.
The formula assumes the beam behaves elastically within the proportionality limit.
E is the Young's Modulus and I is the Area Moment of Inertia.
Predictable structural behavior
Easy calculation for standard load cases
Assumes material homogeneity
Applicable only for prismatic beams (constant EI)
Structural design of building floor beams
Bridge girders under specific point loads
The expression 48EIWl3 (Option B) represents the maximum deflection at the center, not the slope.
The expression 384EI5wl4 (Option D) is the formula for maximum deflection in a simply supported beam with a Uniformly Distributed Load (UDL).
C is correct — The slope at the ends of a simply supported beam under a central point load is 16EIWl2.
Always distinguish between slope (units of radians) and deflection (units of length); slope formulas will always have l2 in the numerator, while deflection formulas have l3 or l4.