Post-impact fatigue of cross-plied, through-the-thickness reinforced carbon/expoxy composites
By: by Thomas E. Serdinak.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA-TM -- 110625.; NASA technical memorandum -- 110625.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Epoxy matrix composites.; Fatigue (Materials); Fatigue tests.; Impact damage.; Reinforcing fibers.; Stress-strain relationships.; Woven composites.
Other titles: Post impact fatigue of cross plied, through the thickness reinforced carbon/expoxy composites.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0033-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 2 microfiches.