Center Deflection Formula:
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The center deflection formula calculates the maximum deflection of a simply supported aluminum angle beam under a central point load. This formula is derived from beam theory and is widely used in structural engineering.
The calculator uses the center deflection formula:
Where:
Explanation: The formula calculates the maximum deflection at the center of a simply supported beam when a force is applied at its midpoint.
Details: Accurate deflection calculation is crucial for structural design, ensuring that aluminum angle beams will not deflect beyond acceptable limits under expected loads.
Tips: Enter force in newtons, length in meters, elastic modulus in pascals, and moment of inertia in meters to the fourth power. All values must be positive.
Q1: What is the typical elastic modulus for aluminum?
A: The elastic modulus for aluminum is typically around 69 GPa (69 × 10⁹ Pa), but can vary slightly depending on the specific alloy.
Q2: How do I calculate moment of inertia for an aluminum angle?
A: Moment of inertia depends on the specific dimensions and orientation of the angle. Standard values can be found in engineering handbooks or calculated using geometric formulas.
Q3: What are acceptable deflection limits?
A: Acceptable deflection limits vary by application, but a common rule is to limit deflection to L/360 for floors and L/240 for roofs under live loads.
Q4: Does this formula work for other materials?
A: Yes, the formula works for any homogeneous, isotropic material behaving elastically, but you must use the appropriate elastic modulus for that material.
Q5: What if the load is not at the center?
A: This calculator is specifically for central point loads. For other load configurations, different formulas must be used.