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Deflection of Simply Supported Beam

Deflection of Simply Supported Beam
\[\delta=\frac{PL^{3}}{48EI}\]

Variables

delta[δ]maximum midspan deflection (m)
Pconcentrated load at midspan (N)
Lbeam span length (m)
EYoung's modulus (Pa)
Isecond moment of area (m⁴)

Description

What is this formula?


The Deflection of Simply Supported Beam formula calculates the maximum vertical deflection produced by a concentrated load applied at the center of a simply supported beam.


Deflection is often a governing design criterion because excessive deformation can affect serviceability even when stresses remain below allowable limits.


When to use it


Use this formula when analyzing:


- Steel beams

- Reinforced concrete beams

- Timber beams

- Floor joists

- Bridge girders


with a single concentrated load acting at midspan.


Example


A simply supported steel beam carries a centered load of 20 kN.


Data:


P = 20,000 N

L = 5 m

E = 200,000,000,000 Pa

I = 8×10⁻⁵ m⁴


Formula:


δ = PL³/(48EI)


Substitution:


δ = (20,000 × 5³)/(48 × 200,000,000,000 × 8×10⁻⁵)


δ = 0.003255 m


Result:


δ = 3.26 mm


Applications


- Structural serviceability checks

- Building floor design

- Bridge engineering

- Steel structures

- Concrete structures

- Timber engineering


Note


This equation applies to a simply supported beam subjected to a single concentrated load at midspan and assumes linear elastic behavior. Different loading conditions such as distributed loads, multiple loads, cantilevers, or continuous beams require different deflection equations.

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