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A simply supported beam of span l, carrying point load W at centre of span, deflection at centre will be
384EI5wl4тАЛ
48EIWl3тАЛ
24EIwl3тАЛ
16EIWl2тАЛ
48EIWl3тАЛ
For a simply supported beam of span l subjected to a central point load W, the maximum deflection occurs at the center. This deflection is determined using the double integration method or Macaulay's method, resulting in the standard formula ╬┤=48EIWl3тАЛ.
For a simply supported beam of span l subjected to a central point load W, the maximum deflection occurs at the center. This deflection is determined using the double integration method or Macaulay's method, resulting in the standard formula ╬┤=48EIWl3тАЛ.
╬┤maxтАЛ=48EIWl3тАЛ тАФ Maximum deflection at center
╬╕=16EIWl2тАЛ тАФ Slope at supports
The beam undergoes bending due to the applied moment induced by the point load. The curvature ╬║ is related to the bending moment M by the elastic curve equation dx2d2yтАЛ=EIMтАЛ. Integrating this equation twice with appropriate boundary conditions at the supports (where deflection y=0 at x=0 and x=l) yields the deflection at any point x, which peaks at x=l/2.
Maximum deflection occurs at the location of the point load.
E is the Young's Modulus and I is the Moment of Inertia.
The deflection is inversely proportional to the flexural rigidity EI.
Standardized design parameter for structural stiffness.
Simple derivation using Euler-Bernoulli beam theory.
Applicable only for linear elastic behavior.
Assumes small deflections (small angle approximation).
Civil structural design of floor beams.
Mechanical design of drive shafts and load-bearing members.
Option A: 384EI5wl4тАЛ represents the deflection of a simply supported beam under a Uniformly Distributed Load (UDL).
Option C: 24EIwl3тАЛ is a dimensional variant, not standard for this case.
Option D: 16EIWl2тАЛ relates to the slope at the support for a central point load, not deflection.
B is correct тАФ The deflection at the center of a simply supported beam with a central point load W is given by 48EIWl3тАЛ.
Remember that UDL produces a higher power of length (l4) in the numerator, while point loads produce l3.