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FASTRAN IIFatigue Crack Growth Structural Analysis (FASTRAN II) predicts growth of crack as function of history of cyclic loads until either crack attains desired size or failure occurs. Based on plasticity-induced closure behavior of cracks in metallic materials and accounts for such load-interaction effects as retardation and acceleration, under variable-amplitude loading. Written in standard FORTRAN 77. Other versions available upon request.
Document ID
19930000781
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Newman, James C., Jr.
(NASA Langley Research Center, Hampton, VA.)
Date Acquired
August 16, 2013
Publication Date
December 1, 1993
Publication Information
Publication: NASA Tech Briefs
Volume: 17
Issue: 12
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-14865
LAR-14944
ISSN: 0145-319X
Report Number: LAR-14865
Report Number: LAR-14944
Accession Number
93B10781
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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