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Unformatted text preview: he beam. The problem is also solved using tapered
sections beam elements (BEAM188). Results Comparison
SHELL63 Deflection, in
(Stress1)max, psi BEAM44 Deflection, in
(Stress1)max, psi BEAM188 Deflection, in
(Stress1)max, psi 1–86 ANSYS Ratio -0.042667 -0.042667 1.000 1600.00 1600.4 1.000 -0.042667 -0.043109 1.010 1600.00 1600.00 1.000 -0.042667 -0.042792 1.003 1600.00 1599.966 1.000 ANSYS Verification Manual . ANSYS Release 9.0 . 002114 . © SAS IP, Inc. VM35: Bimetallic Layered Cantilever Plate with Thermal Loading
Reference: R. J. Roark, W. C. Young, Formulas for Stress and Strain, 5th Edition, McGrawHill Book Co., Inc., New York, NY, 1975, pp. 113-114. Analysis Type(s): Static Analysis (ANTYPE = 0) Element Type(s): Nonlinear Layered Structural Shell Elements (SHELL91) Input Listing: vm35.dat Test Case
A cantilever beam of length , width w, and thickness t is built from two equal thickness layers of different
metals. The beam is stress free at Tref. The beam is fixed at the centerline of one end (X = 0, Y = w/2), and subjecte...
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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.
- Spring '09
- The Land