# Cantilever Beams

## Maximum reaction, deflection and moment - single and uniform loads

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### Cantilever Beam - Single Load

#### Maximum Reaction

can be expressed as:

*R _{A} = F (1a)*

*where *

*R _{A} = reaction force in A (N, lb)*

*F = single acting force in B (N, lb)*

#### Maximum Moment

can be expressed as

*M _{A} = - F a (1b)*

*where *

*M _{A} = maximum moment in A (N.m, N.mm, lb.in)*

*a = length between A and B (m, mm, in)*

#### Maximum Deflection

at the end of the cantilever beam can be expressed as

*δ _{C} = (F a^{3} / (3 E I)) (1 + 3 b / 2 a) (1c)*

*where *

*δ _{C} = maximum deflection in C (m, mm, in)*

*E = modulus of elasticity (N/m ^{2} (Pa), N/mm^{2}, lb/in^{2} (psi))*

*I = moment of Inertia (m ^{4}, mm^{4}, in^{4}) *

*b = length between B and C (m, mm, in)*

#### Maximum Deflection

at the action of the single force can be expressed as

*δ _{B} = F a^{3} / (3 E I) (1d)*

*where *

*δ _{B} = maximum deflection in B (m, mm, in)*

* *

#### Cantilever Beam - Single Load Calculator

A generic calculator - use metric values based on m or mm, or imperial values based on inches. Default typical values are in metric mm.

### Cantilever Beam - Uniform Load

#### Maximum Reaction

can be expressed as:

*R _{A} = q L (2a)*

*where *

*R _{A} = reaction force in A (N, lb)*

*q = uniform load (N/m, N/mm, lb/in)*

*L = length of cantilever beam (m, mm, in)*

#### Maximum Moment

can be expressed as

*M _{A} = - q L^{2} / 2 (2b)*

#### Maximum Deflection

can be expressed as

*δ _{B} = q L^{4} / (8 E I) (2c)*

*where *

*δ _{B} = maximum deflection in B (m, mm, in)*

#### Cantilever Beam - Uniform Load Calculator

A generic calculator - use metric values based on m or mm, or imperial values based on inches. Default typical values are in metric mm.

### More than One Point Load and/or Uniform Load acting on a Cantilever Beam

With more than one point load and/or uniform load - the resulting maximum moment in A and resulting maximum deflection in B can be calculated by summarizing the maximum moment in A and maximum deflection in B for each point and/or uniform load.

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