Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue
By: Timothy W. Coats, Charles E. Harris.
Contributors: Harris, Charles E.; United States. National Aeronautics and Space Administration.
Series: NASA-TM -- 111921.; NASA technical memorandum -- 111921.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Aircraft structures.; Finite element method.; Resin matrix composites.; Crack propagation.; Stiffness.; Delaminating.; Fiber composites.
Notes: Shipping list no.: 98-0599-M.

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