Through-the-thickness fatigue crack closure behavior in an aluminum alloy /

Bibliographic Details
Main Author:	Dawicke, D. S.
Corporate Author:	Langley Research Center
Other Authors:	Newman, J. C., Grandt, A. F. (Alten F.), 1945-
Format:	Government Document Microform Book
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [1990]
Series:	NASA technical memorandum ; 102590.
Subjects:	Aluminum alloys > Fatigue. Aluminum alloys. Crack closure. Crack propagation. Fatigue (Materials) Stress intensity factors. Thickness.
Online Access:	https://purl.fdlp.gov/GPO/LPS62877

Description
Item Description:	Cover title. "January 1990." Microform.
Physical Description:	6 pages : illustrations 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.
Bibliography:	Includes bibliographical references (page 5).