Structural Engineering

Beam Deflection: Uniform Distributed Load

Calculates the maximum center-span elastic deflection of a simply supported structural beam subjected to a uniform distributed load (UDL).

\[ \delta_{max} = \frac{5 \cdot w \cdot L^4}{384 \cdot E \cdot I} \]
Plain Text Formula: delta_max = (5 * w * L^4) / (384 * E * I)

📐 Variable Definitions & Parameters

Symbol Variable Name Standard Unit Physical Definition
\[ \delta_{max} \] Mid-Span Deflection meters (m) or mm Maximum downward vertical displacement at x = L/2
\[ w \] Uniform Distributed Load N/m or kN/m Total continuous load per unit length
\[ L \] Clear Span Length meters (m) Distance between support pin and roller
\[ E \] Young's Modulus Pascals (Pa) Elastic modulus of beam material
\[ I \] Moment of Inertia m⁴ Moment of inertia about the horizontal bending axis

💡 Worked Engineering Example

Problem Statement:

A steel beam (E=200 GPa, I=8,000 cm⁴) spans 6 meters under a load w=15 kN/m. Find center deflection.

Step-by-Step Solution:

  1. Convert I: 8,000 cm⁴ = 8e-5 m⁴
  2. w = 15,000 N/m, L = 6 m
  3. Numerator: 5 * 15,000 * 6^4 = 5 * 15,000 * 1,296 = 97,200,000
  4. Denominator: 384 * 200e9 * 8e-5 = 6,144,000,000
  5. Deflection = 97,200,000 / 6,144,000,000 = 0.01582 m = 15.82 mm
🎯 Result: Mid-span deflection is 15.82 mm, which satisfies the standard L/360 deflection limit (6,000 / 360 = 16.67 mm).
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