Original paper
Post-buckling failure evaluation method of integrated composite stiffened panels under uniaxial compression
Abstract
A post-buckling failure evaluation method of integrated composite stiffened panels is required for improving the structure design of composite stiffened panels effectively in the aircraft structure design under uniaxial compression.Finite element models were built using commercial finite element software ABAQUS for the study of the failure evaluation method of integrated composite stiffened panels under uniaxial compression at the post-buckling...
Paper Details
Title
Post-buckling failure evaluation method of integrated composite stiffened panels under uniaxial compression
Published Date
Jan 1, 2014
Journal
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Notes
History