Refer to the plate with a hole example, which shown how to apply structural loads without referring to coefficients.
Boundary Conditions for plane stress
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I do not fully understand how to implement boundary conditions to solve my PDE (Plane stress).
Can somebody explain me how I can use BC properly?
Problem: clamped beam (boundary condition: Dirichlet) with outward load of 100 N/m. The rest of beam has Neumann as boundary condition. What do coefficients means in both conditions?
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