Progressive damage analysis of laminated composite (PDALC)
Subtitle: (a computational model implemented in the NASA COMET finite element code) version 2.0
By: Timothy W. Coats ... [et al.].
Contributors: Coats, Timothy W.; Langley Research Center.
Series: NASA/TM -- 1998-208718.; NASA technical memorandum -- 208718.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Laminates.; Fiber composites.; Residual strength.; Damage assessment.; Finite element method.; Structural analysis.; Failure analysis.; Fracture mechanics.
Other titles: Computational model implemented in the NASA COMET finite element code, version 2.0.
Notes: Shipping list no.: 99-0559-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1999] 1 microfiche.