Computational simulation of damage progression of composite thin shells subjected to mechanical loads

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National Aeronautics and Space Administration, National Technical Information Service, distributor , [Washington, D.C, Springfield, Va
Thin walled shells., Graphite-epoxy composites., Internal pressure., Axial loads., Fracturing., Crack propagation., Computer programs., Composite struct
StatementP.K. Gotsis, C.C. Chamis, L. Minnetyan.
SeriesNASA-TM -- 112531., NASA technical memorandum -- 112531.
ContributionsChamis, C. C., Minnetyan, L., United States. National Aeronautics and Space Administration.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL15497685M

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