Analysis of matrix cracking and local delamination in (O/[theta]-[theta])s[subscript] graphite epoxy laminates under tension load
By: S.A. Salpekar and T.K. O'Brien.
Contributors: O'Brien, T. Kevin.; United States. Army Aviation Research and Technology Activity.; Langley Research Center.
Series: NASA technical memorandum -- 104062.; AVSCOM technical report -- 91-B-002.; AVSCOM technical report -- 91-B-2.
Publisher: National Aeronautics and Space Administration, Langley Research Center; US Army Aviation Systems Command, Aviation R&T Activity; National Technical Information Service, distributor
Published: 1991
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Composite materials -- Delamination.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.