Description Find the meridional stress and the hoop stress at point B shown in Figure 1. Reference Analysis type Linear Static Analysis Technologies used Geometry Load assumptions Uniform internal pressure of 1.0 MPa. Boundary conditions Axisymmetric about rq plane at y=0, i.e. around the waist circle through B: Material properties Isotropic, E = 210 GPa, ν […]
Description Find the displacement in x- direction of point A of hemisphere shown in Figure 1. Reference Analysis type Linear Static Analysis Technologies used Geometry Load assumptions Concentrated radial loads of 2 kN outward at A, inward at C. Boundary conditions Material properties Isotropic, E = 68.25 GPa, ν = 0.3 Computation target Displacement in
Description Find the outer (convex) surface tangential (q – q) stress at point E (refer below figure) of cylindrical shell with two load casesas follow. Reference Analysis type Linear Static Analysis Technologies used Geometry Load assumptions Boundary conditions Material properties Isotropic, E = 210 GPa, ν = 0.3 Computation target Results Case 1 Case 2
Description Calculate the tangential edge stress (σyy) at point D (as indicated in the figure below) of an elliptical membrane under uniform outward pressure. Reference Analysis type Linear Static Analysis Technologies used Geometry Load assumptions Uniform outward pressure of 10 MPa at outer edge BC, Inner curved edge AD unloaded. Boundary conditions Material properties E
