Constant amplitude and post-overload fatigue crack growth behavior in PM aluminum alloy AA 8009
By: A.P. Reynolds.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 104132.
Publisher: National Aeronautics and Space Administration, Langley Research Center, [1991]
Published: 1991
Place of publication: Hampton, Va
Language: eng
Format: Microform
Subjects: Aluminum alloys.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-0453-M.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1991. 1 microfiche.