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101 0 $aeng
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181   $ctxt$2rdacontent
182   $cc$2rdamedia
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200 10$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.
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996   $aSimulation of crack propagation in engine rotating components under variable amplitude loading$93522560
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