Stress ratio effects on crack opening loads and crack growth rates in aluminum alloy 2024
By: William T. Riddell and Robert S. Piascik.
Contributors: Piascik, Robert S.; Langley Research Center.
Series: [NASA technical memorandum] -- NASA/TM-1998-206929.; NASA technical memorandum -- 206929.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1998
Place of publication: Hampton, Va; Springfield, VA
Language: eng
Format: Microform
Subjects: Crack propagation.; Stress ratio.; Aluminum alloys.; Crack closure.; Fatigue (Materials).
Notes: Shipping list no.: 99-0618-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1998] 1 microfiche.