Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures /

Bibliographic Details
Main Author:	Jackson, Karen E.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; 1985.
Series:	AVSCOM technical report ; 85-B-7. NASA technical paper ; 2520.
Subjects:	Airplanes > Fuselage > Testing. Aluminum compounds > Testing. Epoxy compounds > Testing. Abrasion. Aluminum. Crash landing. Graphite-epoxy composites. Panels. Runways. Skid landings. Skin (Structural member) Transport aircraft.
Online Access:	https://purl.fdlp.gov/GPO/LPS54443

Description
Item Description:	Microform.
Physical Description:	1 volume Also available via Internet from the NASA web site. Address as of 10/4/04: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19860003848%5F1986003848.pdf; current access is available via PURL.
Bibliography:	Includes bibliographical references.