Abrasion behavior of aluminum and composite skin coupons, stiffened skins, and stiffened panels representative of transport airplane structures
By: Karen E. Jackson.
Contributors: United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Series: NASA technical paper -- 2520.; AVSCOM technical report -- 85-B-7.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service
Published: 1985
Place of publication: [Washington, D.C.]; Springfield, Va
Language: eng
Format: Microform
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.
Notes: Includes bibliographical references.

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.

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