Dynamic delamination buckling in composite laminates under impact loading
Subtitle: computational simulation
By: Joseph E. Grady, Christos C. Chamis, and Robert A. Aiello ; prepared for the Second Symposium on Composite Materials, Fatigue and Fracture, sponsored by the American Society for Testing and Materials, Cincinnati, Ohio, April 26-30, 1987.
Contributors: Chamis, C. C.; Aiello, Robert A.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 100192.
Publisher: National Aeronautics and Space Administration; For sale by the National Technical Information Service
Published: 1987
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
Number of pages: 12
Subjects: Composite materials -- Delamination.; Buckling.; Composite materials.; Computerized simulation.; Delaminating.; Dynamic loads.; Impact loads.
Notes: Cover title.

Distributed to depository libraries in microfiche.

Includes bibliographical references (p. 6-7).

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche : negative.