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Aluminum Tube Deflection Calculator

Beam Deflection Formula:

\[ \delta = \frac{F L^3}{3 E I} \]

N
m
Pa
m⁴

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1. What is Beam Deflection?

Beam deflection refers to the displacement of a beam under load. For aluminum tubes, understanding deflection is crucial for structural design and ensuring components meet safety and performance requirements.

2. How Does the Calculator Work?

The calculator uses the beam deflection formula:

\[ \delta = \frac{F L^3}{3 E I} \]

Where:

Explanation: This formula calculates the maximum deflection of a cantilever beam with a point load at the free end. The deflection increases with the cube of the beam length and linearly with the applied force.

3. Importance of Deflection Calculation

Details: Accurate deflection calculation is essential for structural engineering, ensuring that aluminum tubes can withstand expected loads without excessive bending that could lead to failure or performance issues.

4. Using the Calculator

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 and non-zero.

5. Frequently Asked Questions (FAQ)

Q1: What is the typical elastic modulus for aluminum?
A: Aluminum typically has an elastic modulus of approximately 69 GPa (69 × 10⁹ Pa), though this can vary by alloy.

Q2: How do I calculate moment of inertia for a tube?
A: For a circular tube, \( I = \frac{\pi}{64}(D_o^4 - D_i^4) \), where \( D_o \) is outer diameter and \( D_i \) is inner diameter.

Q3: What are acceptable deflection limits?
A: Acceptable deflection depends on application, but common limits are L/360 for floors and L/240 for roofs, where L is span length.

Q4: Does this formula work for other materials?
A: Yes, this formula applies to any homogeneous, isotropic material behaving elastically, but the elastic modulus will differ.

Q5: What if the load is distributed instead of point load?
A: For distributed loads, different deflection formulas apply. This calculator is specifically for point loads at the free end of cantilever beams.

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