Center Deflection Formula:
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The maximum deflection formula for a simply supported aluminum beam with a point load at the center calculates the vertical displacement at the midpoint of the beam. This is crucial for structural engineering applications to ensure beams don't deflect beyond acceptable limits.
The calculator uses the center deflection formula:
Where:
Explanation: The formula shows that deflection increases with the cube of beam length and linearly with load, while decreasing with higher material stiffness (E) and cross-sectional stiffness (I).
Details: Calculating beam deflection is essential for structural design to ensure safety, serviceability, and compliance with building codes. Excessive deflection can cause cracking, vibration issues, and user discomfort.
Tips: Enter all values in consistent SI units. For aluminum, typical modulus of elasticity is around 69 GPa (69 × 10⁹ Pa). Moment of inertia depends on the cross-sectional shape of the beam.
Q1: What is the typical modulus of elasticity for aluminum?
A: For most aluminum alloys, E is approximately 69 GPa (69 × 10⁹ Pa), though it varies slightly by alloy type.
Q2: How do I calculate moment of inertia for different beam shapes?
A: Common formulas: Rectangle (bh³/12), Circle (πd⁴/64), I-beam (complex calculation based on dimensions).
Q3: What are acceptable deflection limits?
A: Building codes typically limit deflection to L/360 for live loads and L/240 for total loads, where L is span length.
Q4: Does this formula work for distributed loads?
A: No, this is specifically for a single point load at center. Distributed loads have different deflection formulas.
Q5: How does aluminum compare to steel in deflection?
A: Aluminum has about 1/3 the stiffness of steel (E ≈ 69 GPa vs 200 GPa), so aluminum beams will deflect more under the same load.