Maximum Deflection. at the end of the cantilever beam can be expressed as. δC = (F a3 / (3 E I) (1 + 3 b / 2 a) (1c) where. δC = maximum deflection in C (m, mm, in) E
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This article will attempt to provide a clearer understanding of beam deflection formulas and their use. Simply stated these formulas show how much beams will change their shape and
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The basic equation in beam theory is: Where you is displacement, E is Young's modulus ( a measure of how stiff the beam material is), I is the moment of inertia of the beam crosssection
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