Through-the-thickness fatigue crack closure behavior in an aluminum alloy
By: D.S. Dawicke, J.C. Newman, Jr., and A.F. Grandt, Jr.
Contributors: Newman, J. C.; Grandt, A. F. 1945-; Langley Research Center.
Series: NASA technical memorandum -- 102590
Publisher: National Aeronautics and Space Administration, Langley Research Center; For sale by the National Technical Information Service
Published: 1990
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aluminum alloys -- Fatigue.; Aluminum alloys.; Crack closure.; Crack propagation.; Fatigue (Materials); Stress intensity factors.; Thickness.
Notes: Cover title.

"January 1990."

Includes bibliographical references (p. 5).

Also available via Internet from the NASA Technical Report Server web site. Address as of 8/18/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900011111%5F1990011111.pdf ; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.