Choose a Boundary Condition and Calculate! |
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Euler-Bernoulli Beam Equation |
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The out-of-plane displacement w of a beam is governed by the Euler-Bernoulli Beam Equation,
![]() where p is the distributed loading (force per unit length) acting in the same direction as y (and w), E is the Young's modulus of the beam, and I is the area moment of inertia of the beam's cross section. If E and I do not vary with x along the length of the beam, then the beam equation simplifies to,
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Origin of the Beam Equation |
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The Euler beam equation arises from a combination of four distinct subsets of beam theory: the kinematic, constitutive, force resultant, and equilibrium definition equations.
The outcome of each of these segments is summarized here: |
Kinematics: | ![]() |
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Constitutive: | ![]() |
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Resultants: |
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Equilibrium: |
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To relate the beam's out-of-plane displacement w to its pressure loading p, we combine the results of the four beam sub-categories in the order shown, |
Kinematics | -> | Constitutive | -> | Resultants | -> | Equilibrium | = | Beam Equation |
We'll demonstrate this hierarchy by working backwards. We first combine the 2 equilibrium equations to eliminate V,
![]() Next replace the moment resultant M with its definition in terms of the direct stress s,
![]() Use the constitutive relation to eliminate s in favor of the strain e, and then use kinematics to replace e in favor of the normal displacement w,
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![]() As a final step, recognizing that the integral over y2 is the definition of the beam's area moment of inertia I,
![]() allows us to arrive at the Euler-Bernoulli beam equation,
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