1981 pp 284 287 static analysis antype 0 4 node

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Unformatted text preview: creased mesh refinement on the percent energy error norm. Figure C1.1 Built-in Plate Problem Sketch Material Properties E = 1 x 107 psi υ = 0.3 Geometric Properties a = 10 in t = 1 in Parameter Definitions N1 = no. elements along each horizontal edge N2 = no. elements through thickness Loading and Boundary Conditions At X = a/2, UX = 0 At x = a/2 and Z = 0, UZ = 0 At Y = a/2, UY = 0 At Y = a/2 and Z = 0, UZ = 0 At X = 0, UX = 0 At Y = 0, UY = 0 At Z = 0, UX = UY = 0 At Z = -t/2, P = -500 ANSYS Verification Manual . ANSYS Release 9.0 . 002114 . © SAS IP, Inc. 2–5 Benchmark C1 Figure C1.2 Representative Mesh Options Solution Information Table C1.1 Target Solution ETYP N1 N2 95 25 10 DOF % Error Norm 45708 UZ(1), in SX(2), ksi SX(3), ksi 10 -.0172 -32.124 14.465 Table C1.2 Results Comparison Ratio ETYP N1 N2 45 3 1 45 6 1 2–6 % Error Norm UZ(1) SX(2) SX(3) 96 57 .925 .461 .983 294 33 .961 .663 .985 DOF ANSYS Verification Manual . ANSYS Release 9.0 . 002114 . © SAS IP, Inc. Benchmark C1 Ratio % Error No...
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This note was uploaded on 12/09/2010 for the course DEPARTMENT E301 taught by Professor Kulasinghe during the Spring '09 term at University of Peradeniya.

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