Experimental verification of a progressive damage model for composite laminates based on continuum damage mechanics
By: Timothy William Coats.
Contributors: Langley Research Center.
Series: NASA contractor report -- 195020.; NASA contractor report -- NASA CR-195020.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Continuum mechanics.; Continuum modeling.; Cracks.; Delaminating.; Graphite-epoxy composites.; Impact damage.; Laminates.; Load tests.; Mathematical models.; Matrix materials.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0615-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 2 microfiches.