Computational simulation of damage progression of composite thin shells subjected to mechanical loads
By: P.K. Gotsis, C.C. Chamis, L. Minnetyan.
Contributors: Chamis, C. C.; Minnetyan, L.; United States. National Aeronautics and Space Administration.
Series: NASA-TM -- 112531.; NASA technical memorandum -- 112531.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Thin walled shells.; Graphite-epoxy composites.; Internal pressure.; Axial loads.; Fracturing.; Crack propagation.; Computer programs.; Composite structures.
Notes: Shipping list no.: 98-0818-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.