Fourth-Order Euler-Bernoulli Elastic Beam Deflection
Euler-Bernoulli beam theory governs flexural members where plane sections remain plane and normal to the longitudinal centroidal axis under transverse loading. The fundamental governing fourth-order differential equation relating transverse displacement $w(x)$ to distributed load $q(x)$ is:
EI * (d⁴w / dx⁴) = q(x)Direct Integration for Simply Supported Beam under Uniform Load:
For a simply supported beam of span $L$ subjected to a continuous uniform downward load $w = q_0$:
- Shear Force Function $V(x)$:V(x) = -EI * (d³w / dx³) = q₀ * (L / 2 - x)
- Bending Moment Function $M(x)$:M(x) = -EI * (d²w / dx²) = (q₀ / 2) * (L * x - x²)Boundary Conditions: M(0) = 0, M(L) = 0. Maximum moment at mid-span: M_max = q₀ * L² / 8.
- Angular Rotation Slope $\theta(x)$:θ(x) = dw/dx = (q₀ / (24 * E * I)) * (2x³ - 6Lx² + 4L³)Boundary Condition by symmetry: θ(L/2) = 0. End rotations: θ(0) = q₀L³ / (24EI), θ(L) = -q₀L³ / (24EI).
- Transverse Elastic Deflection Curve $w(x)$:w(x) = (q₀ * x / (24 * E * I)) * (L³ - 2 * L * x² + x³)Boundary Conditions: w(0) = 0, w(L) = 0.
• w = Distributed load per unit length (lbf/in or kN/m)
• L = Clear span length between supports (in or mm)
• E = Modulus of elasticity of structural material (psi or MPa)
• I = Second moment of area / moment of inertia of section (in⁴ or mm⁴)
• Code Limit: Residential live load deflection criterion: δ_allow = L / 360; Total load: δ_allow = L / 240.