Cantilever Beam Deflection Formula:
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The cantilever beam deflection formula calculates the maximum deflection at the free end of a beam fixed at one end and loaded at the other. For aluminum profiles, this helps engineers determine how much a structural element will bend under specific loads.
The calculator uses the cantilever beam deflection formula:
Where:
Explanation: The formula shows that deflection increases with the cube of the beam length and is inversely proportional to both the elastic modulus and moment of inertia.
Details: Accurate deflection calculation is crucial for structural design, ensuring that aluminum profiles maintain their integrity and functionality under expected loads without excessive bending.
Tips: Enter load in Newtons, length in millimeters, elastic modulus in MPa (69000 MPa typical for aluminum), and moment of inertia in mm⁴. All values must be positive.
Q1: What is the typical elastic modulus for aluminum?
A: The elastic modulus for aluminum alloys typically ranges from 68,000 to 71,000 MPa, with 69,000 MPa being a common average value.
Q2: How do I find the moment of inertia for my aluminum profile?
A: Moment of inertia values are typically provided by the manufacturer and depend on the specific cross-sectional shape and dimensions of the profile.
Q3: What are acceptable deflection limits?
A: Acceptable deflection depends on the application. Common limits range from L/180 to L/360 for structural elements, where L is the span length.
Q4: Does this formula account for distributed loads?
A: No, this specific formula is for a point load at the free end. Different formulas are used for distributed loads along the beam.
Q5: Can this calculator be used for materials other than aluminum?
A: Yes, but you must use the appropriate elastic modulus value for the specific material being calculated.