0 260 ansys 317 258 ratio 1056 0994 1 target results

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Unformatted text preview: § HIG3EF8CDB@8 753!0 A 9 6 4 21 ( $" )%#! Geometric Properties = 10 in h = 2 in d = 1 in ¦  & $" '%#!   Material Properties E = 30 x 106 psi υ = 0.0 Loading Case 1, M = 2000 in-lb Case 2, F = 300 lb Analysis Assumptions and Modeling Notes The stiffness matrix formed in the first load step is also used in the second load step (automatically determined by ANSYS). The end moment is represented by equal and opposite forces separated by a distance h. The bending stress is obtained from face stresses on element 1. ANSYS Verification Manual . ANSYS Release 9.0 . 002114 . © SAS IP, Inc. 1–47 VM16 Results Comparison Target 1. 1–48 Deflection, in 0.00500 0.00500 1.000 3000 3000[1] 1.000 Deflection, in 0.00500 0.00505 1.010 StressBend , psi Case 2 Ratio StressBend , psi Case 1 ANSYS 4050 4050[1] 1.000 S(PAR) in face printout for element 1 in element solution printout. ANSYS Verification Manual . ANSYS Release 9.0 . 002114 . © SAS IP, Inc. VM17: Snap-Through Buckling of a Hinged Shell Overview Reference: C. C. Chang, “Periodically Restarted Quasi-Newton Updates in Constant ArcLength Method”, Computers and Struct...
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