HyperSizer Published Paper   (14 pages)

"Thermoelastic Formulation of Stiffened, Unsymmetric Composite Panels for Finite Element Analysis of High Speed Aircraft"

Presented at the 35th AIAA/ASME/ASCE/AHS/ACS Structures, Dynamics, & Materials Conference, Hilton Head, SC, April 18-20, 1994.

Keywords: coupling between in-plane shear and bending-twisting, A33, B33, D33, D22, transverse bending, shear flow, closed cell, torsional rigidity, warpage, increased panel buckling, membrane-bending coupling, unsymmetric sections, curvature, coarse meshed 2-D planar FEM, hat-shaped corrugated, validate, verify, 3-D FEA, thermoelastic formulation

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aiaa94_1579_added_formulations_hypersizer.pdf - 557 Kb

• Format - PDF

• Date Posted - April 1994

• File Size - 557 Kb

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