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CivilStructural Mechanics-II
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A simply supported beam of span l, carrying point load W at centre of span, deflection at centre will be

A

5wl4384EI\frac{5wlтБ┤}{384EI}384EI5wl4тАЛ

B

Wl348EI\frac{Wl┬│}{48EI}48EIWl3тАЛ

C

wl324EI\frac{wl┬│}{24EI}24EIwl3тАЛ

D

Wl216EI\frac{Wl┬▓}{16EI}16EIWl2тАЛ

Correct Answer

тЪЩя╕П TE тАв Technical Concept & PrincipleCivilStructural Mechanics-II
Option B

Wl348EI\frac{Wl┬│}{48EI}48EIWl3тАЛ

Quick Summary:

For a simply supported beam of span lll subjected to a central point load WWW, 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 ╬┤=Wl348EI\delta = \frac{Wl┬│}{48EI}╬┤=48EIWl3тАЛ.

тЪЩя╕ПTETechnical SolutionConcept & Principle
ЁЯТб Explanation

For a simply supported beam of span lll subjected to a central point load WWW, 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 ╬┤=Wl348EI\delta = \frac{Wl┬│}{48EI}╬┤=48EIWl3тАЛ.

ЁЯФв Key Formulas

╬┤max=Wl348EI\delta_{max} = \frac{Wl┬│}{48EI}╬┤maxтАЛ=48EIWl3тАЛ тАФ Maximum deflection at center

╬╕=Wl216EI\theta = \frac{Wl┬▓}{16EI}╬╕=16EIWl2тАЛ тАФ Slope at supports

тЪЩя╕П Working Principle

The beam undergoes bending due to the applied moment induced by the point load. The curvature ╬║\kappa╬║ is related to the bending moment MMM by the elastic curve equation d2ydx2=MEI\frac{d^2y}{dx┬▓} = \frac{M}{EI}dx2d2yтАЛ=EIMтАЛ. Integrating this equation twice with appropriate boundary conditions at the supports (where deflection y=0y=0y=0 at x=0x=0x=0 and x=lx=lx=l) yields the deflection at any point xxx, which peaks at x=l/2x = l/2x=l/2.

ЁЯУМ Key Points
  • тЦ╕

    Maximum deflection occurs at the location of the point load.

  • тЦ╕

    EEE is the Young's Modulus and III is the Moment of Inertia.

  • тЦ╕

    The deflection is inversely proportional to the flexural rigidity EIEIEI.

тЬЕ Advantages
  • тЦ╕

    Standardized design parameter for structural stiffness.

  • тЦ╕

    Simple derivation using Euler-Bernoulli beam theory.

тЭМ Disadvantages / Limitations
  • тЦ╕

    Applicable only for linear elastic behavior.

  • тЦ╕

    Assumes small deflections (small angle approximation).

ЁЯЫая╕П Applications / Uses
  • тЦ╕

    Civil structural design of floor beams.

  • тЦ╕

    Mechanical design of drive shafts and load-bearing members.

ЁЯУД Additional Information
  • тЦ╕

    Option A: 5wl4384EI\frac{5wlтБ┤}{384EI}384EI5wl4тАЛ represents the deflection of a simply supported beam under a Uniformly Distributed Load (UDL).

  • тЦ╕

    Option C: wl324EI\frac{wl┬│}{24EI}24EIwl3тАЛ is a dimensional variant, not standard for this case.

  • тЦ╕

    Option D: Wl216EI\frac{Wl┬▓}{16EI}16EIWl2тАЛ relates to the slope at the support for a central point load, not deflection.

ЁЯУК Diagram / Illustration
Central Deflection Formula
Wl3Wl^3Wl3
48EI48EI48EI
╬┤max=Wl348EI\delta_{max} = (Wl^3 / 48EI)╬┤maxтАЛ=48EIWl3тАЛ
тЬЕ

B is correct тАФ The deflection at the center of a simply supported beam with a central point load WWW is given by Wl348EI\frac{Wl┬│}{48EI}48EIWl3тАЛ.

Core Concepts Used
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Euler-Bernoulli beam theory Flexural rigidity ($EI$) Boundary conditions in structural mechanics
ЁЯТб EXAM TIP

Remember that UDL produces a higher power of length (l4lтБ┤l4) in the numerator, while point loads produce l3l┬│l3.

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