LEADER 01930oam  2200493   450 
001 9910705825903321
005 20170807141148.0
035   $a(CKB)5470000002454161
035   $a(OCoLC)227901839
035   $a(EXLCZ)995470000002454161
100   $a20080513j199810    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aSimulation of crack propagation in engine rotating components under variable amplitude loading /$fP.J. Bonacuse [and four others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center and U.S. Army Research Laboratory,$dOctober 1998.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v1998-208648
300   $a"October 1998."
300   $a"Prepared for the Symposium of the Applied Vehicle Technology Panel sponsored by the NATO/AGARD, Toulouse, France, May 11-15, 1998."
300   $a"Performing organization: NASA Lewis Research Center and U.S. Army Research Laboratory"--Report documentation page.
300   $a"ARL-MR-418."
320   $aIncludes bibliographical references (page 15).
606   $aCrack propagation$2nasat
606   $aSimulation$2nasat
606   $aRotary wing aircraft$2nasat
606   $aVariable amplitude loading$2nasat
615  7$aCrack propagation.
615  7$aSimulation.
615  7$aRotary wing aircraft.
615  7$aVariable amplitude loading.
700   $aBonacuse$b Peter J.$f1960-$01406621
712 02$aLewis Research Center,
712 02$aU.S. Army Research Laboratory.
801  0$bDTICE
801  1$bDTICE
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910705825903321
996   $aSimulation of crack propagation in engine rotating components under variable amplitude loading$93522560
997   $aUNINA