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

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

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Bibliographic Details
Main Author: Dawicke, D. S
Corporate Author: Langley Research Center
Other Authors: Grandt, A. F (Alten F.), 1945-, Newman, J. C
Format: Government Document Book
Language:English
Published: Hampton, Va. : [Springfield, Va. : National Aeronautics and Space Administration, Langley Research Center ; For sale by the National Technical Information Service, 1990]
Series:NASA technical memorandum ; 102590
Subjects:
Aluminum alloys > Fatigue
Aluminum alloys
Crack closure
Crack propagation
Fatigue (Materials)
Stress intensity factors
Thickness
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100 1 |a Dawicke, D. S 
245 1 0 |a Through-the-thickness fatigue crack closure behavior in an aluminum alloy  |h [microform] /  |c D.S. Dawicke, J.C. Newman, Jr., and A.F. Grandt, Jr 
260 |a Hampton, Va. :  |b National Aeronautics and Space Administration, Langley Research Center ;  |a [Springfield, Va. :  |b For sale by the National Technical Information Service,  |c 1990] 
300 |a 6 p. :  |b ill 
440 0 |a NASA technical memorandum ;  |v 102590 
500 |a Cover title 
500 |a "January 1990." 
504 |a Includes bibliographical references (p. 5) 
530 |a 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 
533 |a Microfiche  |b [Washington, D.C. :  |c National Aeronautics and Space Administration,  |d 1990].  |e 1 microfiche : negative. 
650 0 |a Aluminum alloys  |x Fatigue 
650 7 |a Aluminum alloys  |2 nasat 
650 7 |a Crack closure  |2 nasat 
650 7 |a Crack propagation  |2 nasat 
650 7 |a Fatigue (Materials)  |2 nasat 
650 7 |a Stress intensity factors  |2 nasat 
650 7 |a Thickness  |2 nasat 
700 1 |a Grandt, A. F  |q (Alten F.),  |d 1945- 
700 1 |a Newman, J. C 
710 2 |a Langley Research Center 
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