Failure mechanisms of laminates transversely loaded by bolt push-through /

Bibliographic Details
Main Author:	Waters, William Allen
Corporate Author:	Langley Research Center
Other Authors:	Williams, Jerry G.
Format:	Government Document Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985]
Series:	NASA technical memorandum ; 87603.
Subjects:	Bolted joints. Airplanes > Fuselage. Airframes > Fatigue. Adhesive bonding. Bolts. Composite materials. Failure modes. Fuselages. Interlayers. Laminates. Loads (Forces) Panels. Stiffening. Toughness. Wing panels.
Online Access:	https://purl.fdlp.gov/gPO/LPS85281

Description
Item Description:	Microform.
Physical Description:	1 volume 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.