The effect of resin toughness and modulus on compressive failure modes of quasi-isotropic graphite/epoxy laminates
By: Mohsen M. Sohi, H. Thomas Hahn, and Jerry G. Williams.
Contributors: Hahn, H. Thomas.; Williams, Jerry G.; Langley Research Center.
Series: NASA technical memorandum -- 87604.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1986
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Composite materials -- Testing.; Graphite composites.; Delaminating.; Failure modes.; Graphite-epoxy composites.; Resin matrix composites.
Notes: Also available via Internet from the NTRS web site. Address as of 8/24/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860013176%5F1986013176.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.