A thermodynamically consistent damage model for advanced composites /

Bibliographic Details

Corporate Author:	Langley Research Center
Other Authors:	Maimí, Pere
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2006]
Series:	NASA technical memorandum ; 214282.
Subjects:	Composite materials. Damage. Continuum modeling. Fiber composites. Crack closure. Degradation. Loads (Forces)
Online Access:	https://purl.fdlp.gov/GPO/gpo2935