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01508aam a22003857a 4500 001 1FC42508650B11E6BA021E8ADAD10320 003 SILO 005 20160818010336 008 971211s1997 vau b f000 0 eng d 035 $a (OCoLC)38068914 040 $a GPO $c GPO $d DLC $d MvI $d SILO 074 $a 0830-D (MF) 086 0 $a NAS 1.15:110307 100 1 $a Newman, J. C. 245 10 $a Fatigue-life prediction methodology using small-crack theory $h [microform] / $c J.C. Newman, Jr. and E.P. Phillips, M.H. Swain. 246 3 $a Fatigue life prediction methodology using small crack theory 260 $a Hampton, Va. : $b National Aeronautics and Space Administration, Langley Research Center ; $c 1997] 300 $a 1 v. 440 0 $a NASA technical memorandum $v 110307 500 $a Distributed to depository libraries in microfiche. 500 $a Shipping list no.: 97-0960-M. 533 $a Microfiche. $b [Washington, D.C. : $c National Aeronautics and Space Administration, $d 1997] $e 1 microfiche. 650 7 $a Crack closure. $2 nasat 650 7 $a Fatigue life. $2 nasat 650 7 $a Crack propagation. $2 nasat 650 7 $a Plastic properties. $2 nasat 650 7 $a Stress intensity factors. $2 nasat 650 7 $a Models. $2 nasat 650 7 $a Crack tips. $2 nasat 700 1 $a Phillips, E. P. 700 1 $a Swain, M. H. 710 2 $a Langley Research Center 941 $a 1 952 $l USUX851 $d 20160818054336.0 956 $a http://locator.silo.lib.ia.us/search.cgi?index_0=id&term_0=1FC42508650B11E6BA021E8ADAD10320Initiate Another SILO Locator Search