H macneal r l harder a proposed standard set of

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
This is the end of the preview. Sign up to access the rest of the document.

Unformatted text preview: C Parameter Definition N1 = Element edge length Geometric Properties a = 0.6 m b = 1.0 m c = 0.2 m Loading h = 750 W/m2°C T0 = 0°C T1 = 100°C ANSYS Verification Manual . ANSYS Release 9.0 . 002114 . © SAS IP, Inc. 2–23 Benchmark C6 Figure C6.2 Representative Mesh Options Results Comparison - Triangle Mesh ETYP N1 DOF Temp(°C) Temperature Ratio Quadrilateral Mesh 55[1] .2 24 19.3 1.06 55 .1 77 18.9 1.03 77[1] .2 62 16.4 0.90 77 .1 213 18.7 1.02 Triangle Mesh 35 .2 93 17.9 0.98 35 .1 317 18.3 1.00 55 .2 28 20.9 1.14 2–24 ANSYS Verification Manual . ANSYS Release 9.0 . 002114 . © SAS IP, Inc. Benchmark C6 ETYP N1 DOF Temp(°C) Temperature Ratio 55 .1 88 19.0 1.04 77 .2 93 17.9 0.98 77 .1 317 18.3 1.00 Uniform Triangle Mesh 35[1] 2 77 16.5 0.90 35 .1 273 18.3 1.00 55 .2 24 22.4 1.22 55 .1 77 18.9 1.04 77[1] 2 77 16.5 0.90 77 .1 273 18.3 1.00 1. Test case corresponds to NAFEMS test specification Assumptions, Modeling Notes, and Solution Comments 1. The lower order PLANE55 element co...
View Full Document

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.

Ask a homework question - tutors are online