NASA NTRS · 19890000461
Dynamic Delamination Buckling In Composite Laminates
Abstract
Procedure for mathematical modeling of dynamic delamination buckling and propagation of delamination, with plate bending elements and multipoint constraints, developed and incorporated into finite-element computer program. Predicts time at which delamination buckling occurs, shape of dynamic-buckling mode, and strain-energy-release rate due to extension of delamination crack. Method extended to handle such other defects as transply and edge cracks.
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Grady, Joseph E., Chamis, Christos C., Aiello, Robert A.. 1989-09-01. Dynamic Delamination Buckling In Composite Laminates. https://ntrs.nasa.gov/citations/19890000461
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