Delamination behavior of quasi-isotropic graphite epoxy laminates subjected to tension and torsion loads / J.A. Hinkley and T. K. O'Brien.

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Bibliographic Details
Online Access:	Online Access
Main Authors:	Hinkley, J. A. (Author), O'Brien, T. Kevin (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 1992.
Series:	NASA technical memorandum ; 104181.
Subjects:	American Helicopter Society. Laminates. Torsion.

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Call Number:	NAS 1.15:104181
NAS 1.15:104181	Available