Strength of Materials : Deflection of Beams

By Apoorbo Roy|Updated : August 5th, 2021

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The deformation of a beam is usually expressed in terms of its deflection from its original unloaded position. The deflection is measured from the original neutral surface of the beam to the neutral surface of the deformed beam. The configuration assumed by the deformed neutral surface is known as the elastic curve of the beam.

Slope of a Beam: Slope of a beam is the angle between deflected beam to the actual beam at the same point.

Deflection of Beam: Deflection is defined as the vertical displacement of a point on a loaded beam. There are many methods to find out the slope and deflection at a section in a loaded beam.

The maximum deflection occurs where the slope is zero. The position of the maximum deflection is found out by equating the slope equation zero. Then the value of x is substituted in the deflection equation to calculate the maximum deflection

DIFFERENTIAL EQUATION OF THE DEFLECTION CURVE OF BEAM

Methods of Determining Beam Deflections
Numerous methods are available for the determination of beam deflections. These methods include:

Double Integration Method:

This is most suitable when concentrated or udl over entire length is acting on the beam.A double integration method is a powerful tool in solving deflection and slope of a beam at any point because we will be able to get the equation of the elastic curve.
A double integration method is a powerful tool in solving deflection and slope of a beam at any point because we will be able to get the equation of the elastic curve.

In calculus, the radius of curvature of a curve y = f(x) is given by:

In the derivation of flexure formula, the radius of curvature of a beam is
$ρ = \frac{E I}{M}$

$ρ = \frac{E I}{M}$

If EI is constant, the equation may be written as:
EIy′′=M
where x and y are the coordinates shown in the figure of the elastic curve of the beam under load.

y is the deflection of the beam at any distance x.
E is the modulus of elasticity of the beam,
I represent the moment of inertia about the neutral axis, and
M represents the bending moment at a distance x from the end of the beam.

The product EI is called the flexural rigidity of the beam.

Integrating one time:

The first integration y'(dy/dx) yields the Slope of the Elastic Curve.

Second Integration:

The second integration y gives the Deflection of the Beam at any distance x.

The resulting solution must contain two constants of integration since EI y" = M is of second order.
These two constants must be evaluated from known conditions concerning the slope deflection at certain points of the beam.
For instance, in the case of a simply supported beam with rigid supports, at x = 0 and x = L, the deflection y = 0, and in locating the point of maximum deflection, we simply set the slope of the elastic curve y' to zero

Area Moment Method (Mohr's Method):

Another method of determining the slopes and deflections in beams is the area-moment method, which involves the area of the moment diagram.The moment-area method is a
The moment-area method is a semi graphical procedure that utilizes the properties of the area under the bending moment diagram. It is the quickest way to compute the deflection at a specific location if the bending moment diagram has a simple shape.

Theorems of Area-Moment Method:

Theorem 1
- The angle between the tangent of the deflection curve of two points A and B is equal to the negative area of M/EI diagram between the points.

Theorem 2
- The deviation of B from tangent at A is equal to the negative of the statical moment (or the first moment) with respect to B, of the M/EI
  diagram area between A and B.

Method of Superposition: The method of superposition, in which the applied loading is represented as a series of simple loads for which deflection formulas are available. Then the desired deflection is computed by adding the contributions of the component loads(principle of superposition).

Mostly direct formula is used in questions, hence it is advised to look for the beam deflection formula which are directly asked from this topic rather than going for long derivations.

Deflection for Common Loadings:

Concentrated load at the free end of cantilever beam (origin at A):

Maximum Moment, M =−PL
Slope at end: $θ = \frac{P L^{2}}{2 E I}$
Maximum deflection: $δ = \frac{P L^{3}}{3 E I}$
Deflection Equation ( $y$ is positive downward): $E I y = \frac{P x^{2}}{6} (3 L - x)$

2 .Concentrated load at any point on the span of cantilever beam

Maximum Moment: M= -wa
Slope at end: $θ = \frac{P a^{2}}{2 E I}$
Maximum deflection: $δ = \frac{P a^{3}}{6 E I} (3 L - a)$
Deflection Equation (y is positive downward),
- $E I y = \frac{P x^{2}}{6} (3 a - x) for 0 < x < a$
- $E I y = \frac{P x^{2}}{6} (3 a - x) for 0 < x < a$

Uniformly distributed load over the entire length of cantilever beam

Maximum Moment: $M = - \frac{w_{o} L^{2}}{2}$
Slope at end: $θ = \frac{w_{o} L^{3}}{6 E I}$
Maximum deflection: $δ = \frac{w_{o} L^{4}}{8 E I}$
Deflection Equation ( $y$ is positive downward): $E I y = \frac{w_{o} x^{2}}{120 L} (6 L^{2} - 4 L x + x^{2})$

Triangular load, full at the fixed end and zero at the free end

Maximum Moment: $M = - \frac{w_{o} L^{2}}{6}$
Slope at end: $θ = \frac{w_{o} L^{3}}{24 E I}$
Maximum deflection, $δ = \frac{w_{o} L^{4}}{30 E I}$
Deflection Equation ( $y$ is positive downward): $E I y = \frac{w_{o} x^{2}}{120 L} (10 L^{3} - 10 L^{2} x + 5 L x^{2} - x^{3})$

Moment load at the free end of cantilever beam

Maximum Moment: $M = - M$
Slope at end: $θ = \frac{M L}{E I}$
Maximum deflection: $δ = \frac{M L^{2}}{2 E I}$
Deflection Equation ( $y$ is positive downward): $E I y = \frac{M x^{2}}{2}$

$E I y = \frac{M x^{2}}{2}$

Maximum Moment: $M = \frac{P L}{4}$
Slope at end: θ_A=θ_B= WL²/16EI
Maximum deflection: $δ = \frac{P L^{3}}{48 E I}$
Deflection Equation ( $y$ is positive downward): $E I y = \frac{P x}{12} (\frac{3}{4} L^{2} - x^{2}) for 0 < x < \frac{1}{2} L$

Uniformly distributed load over the entire span of simple beam

Maximum Moment: $M = \frac{w_{o} L^{2}}{8}$
Slope at end: $θ_{L} = θ_{R} = \frac{w_{o} L^{3}}{24 E I}$
Maximum deflection: $δ = \frac{5 w_{o} L^{4}}{384 E I}$
Deflection Equation ( $y$ is positive downward): $E I y = \frac{w_{o} x}{24} (L^{3} - 2 L x^{2} + x^{3})$

9.Triangle load with zero at one support and full at the other support of simple beam

Maximum Moment: $M = \frac{w_{o} L^{2}}{9 \sqrt{3}}$
Slope at end,
- θ_L= 7wL³/360EI
- θ_R= 8wL³/360EI
Maximum deflection: $δ = \frac{2.5 w_{o} L^{4}}{384 E I} at x = 0.519 L$
Deflection Equation ( $y$ is positive downward), $E I y = \frac{w_{o} x}{360 L} (7 L^{4} - 10 L^{2} x^{2} + 3 x^{4})$

Triangular load with zero at each support and full at the midspan of simple beam

Maximum Moment: $M = \frac{w_{o} L^{2}}{12}$
Slope at end, $θ_{L} = θ_{R} = \frac{5 w_{o} L^{3}}{192 E I}$
Maximum deflection: $δ = \frac{w_{o} L^{4}}{120 E I}$
Deflection Equation ( $y$ is positive downward): $E I y = \frac{w_{o} x}{960 L} (25 L^{4} - 40 L^{2} x^{2} + 16 x^{4}) for 0 < x < \frac{L}{2}$

Conjugate Beam method

Support conditions for the real and conjugate beam:

DEFLECTIONS BY CASTIGLIANO'S THEOREM:

Beam Deflection Formula:

Cantilever Beams:

Simply supported Beams:

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