224 Finite Element Analysis and Design 10. Let a uniform cantilevered beam of length Lbe supported at the loaded end so that this end cannot rotate, as shown in the figure. For the given moment of inertia I, Young‟s modulus E, and applied tip load P, calculate the deflection curve v(x) using one beam element. Solution: From the element matrix equation, 11221132222212612606462012612606264LLvFLLLLMEILLvPLMLLLL
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