Failure mechanisms of laminates transversely loaded by bolt push-through
By: William Allen Waters, Jr. and Jerry G. Williams.
Contributors: Williams, Jerry G.; Langley Research Center.
Series: NASA technical memorandum -- 87603.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1985
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Bolted joints.; Airplanes -- Fuselage.; Airframes -- Fatigue.; Adhesive bonding.; Bolts.; Composite materials.; Failure modes.; Fuselages.; Interlayers.; Laminates.; Loads (forces); Panels.; Stiffening.; Toughness.; Wing panels.
Notes: Also available via Internet from the NTRS web site. Address as of 8/23/07: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860004844%5F1986004844.pdf ; current access is available via PURL.

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