Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads
By: J.A. Hinkley 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 -- 104181.; AVSCOM technical report -- 91-B-018.; AVSCOM technical report -- 91-B-18.
Publisher: National Aeronautics and Space Administration, Langley Research Center; US Army Aviation Systems Command, Aviation R&T Activity; National Technical Information Service [distributor]
Published: 1992
Place of publication: Hampton, Va; [St. Louis, Mo.]; [Springfield, Va.?
Language: eng
Format: Microform
Subjects: Composite materials -- Delamination.
Other titles: Delamination behavior of quasi isotropic graphite epoxy laminates subjected to tension and torsion loads.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-1811-M.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1992. 1 microfiche.