A coupled/upcoupled computational scheme for deformation and fatique damage analysis of unidirectional metal-matrix composites
By: Thomas E. Wilt, Steven M. Arnold, and Atef F. Saleeb.
Contributors: Arnold, S. M.; Saleeb, Atef F.; United States. National Aeronautics and Space Administration.
Series: NASA/TM -- 97-207882.; NASA technical memorandum -- 297882.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1998
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Metal matrix composites.; Continuum modeling.; Fatigue (Materials); Finite element method; Stress-strain relationships.
Other titles: Coupled upcoupled computational scheme for deformation and fatique damage analysis of unidirectional metal-matrix composites.
Notes: Shipping list no.: 99-0032-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.