A progressive damage methodology for residual strength predictions of notched composite panels
By: Timothy W. Coats and Charles E. Harris.
Contributors: Harris, Charles E., 1950-; Langley Research Center.
Series: [NASA technical memorandum] -- NASA/TM-1998-207646.; NASA technical memorandum -- 207646.
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: Composite structures.; Crack propagation.; Epoxy matrix composites.; Fractography.; Fracture mechanics.; Fracture strength.; Laminates.; Loads (Forces); Residual strength.
Notes: Shipping list no.: 99-0354-M.

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