Progressive Damage Analysis of Laminated Composite (PDALC)--a computational model implemented in the NASA COMET finite element code
By: David C. Lo ... [et al.].
Contributors: Lo, David C.; Langley Research Center.
Series: NASA technical memorandum -- 4724.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1996
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Residual strength.; Constitutive equations.; Structural analysis.; Finite element method.; Stress distribution.; Laminates.; Composite materials.; Matrix materials.; Cracking (Fracturing)
Other titles: Computational model implemented in the NASA COMET finite element code.
Notes: Shipping list no.: 98-0799-M.

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