Overload and underload effects on the fatigue crack growth behavior of the 2024-T3 aluminum alloy
By: David S. Dawicke.
Contributors: Langley Research Center.
Series: NASA contractor report -- 201668.; NASA contractor report -- NASA CR-201668.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1997
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Fatigue (Materials); Crack propagation; Aluminum alloys; Compression loads
Notes: Shipping list no.: 98-0848-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.