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

Description

Main Author

Jackson, Karen E.

Language(s)

English

Published

[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Subjects

Epoxy compounds > Epoxy compounds / Testing.
Aluminum compounds > Aluminum compounds / Testing.
Airplanes > Airplanes / Fuselage > Airplanes / Fuselage / Testing.

Note

"The objective of this investigation was to compare the friction and wear response of aluminum and graphite-epoxy (Gr-Ep) composite materials when subjected to loading conditions similar to those experienced by the skin panels on the underside of a transport airplane during an emergency sliding landing on a runway surface"--P. 7.

Physical Description

30 p.: ill. ; 28 cm.

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