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001 9910707330203321
005 20161122150351.0
035   $a(CKB)5470000002464218
035   $a(OCoLC)844681397
035   $a(EXLCZ)995470000002464218
100   $a20130526j199610    ua             0
101 0 $aeng
135   $aurbn||||a|a||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine /$fA. Karl Owen, Duane L. Mattern, Dzu K. Le
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Lewis Research Center :$cU.S. Army Research Laboratory,$dOctober 1996.
215   $a1 online resource (9 pages) $cillustrations
225 1 $aNASA technical memorandum ;$v107339
225 1 $aArmy Research Laboratory technical report ;$vARL-TR-1108
300   $aTitle from title screen (viewed July 26, 2016).
300   $a"October 1996"--Report documentation page.
300   $a"Prepared for the 41st Gas Turbine and Aeroengine Congress sponsored by the International Gas Turbine Institute of the American Society of Mechanical Engineers, Birmingham, United Kingdom, June 10-13, 1996."
300   $a"Performing organization: NASA Lewis Research Center and Vehicle Propulsion Directorate, U.S. Army Research Laboratory"--Report documentation page.
300   $a"ASME 96-GT-239."
320   $aIncludes bibliographical references (page 9).
606   $aGas turbine engines$2nasat
606   $aCompressors$2nasat
606   $aFourier analysis$2nasat
606   $aSurges$2nasat
606   $aRotating stalls$2nasat
606   $aModal response$2nasat
606   $aTraveling waves$2nasat
606   $aAircraft engines$2nasat
615  7$aGas turbine engines.
615  7$aCompressors.
615  7$aFourier analysis.
615  7$aSurges.
615  7$aRotating stalls.
615  7$aModal response.
615  7$aTraveling waves.
615  7$aAircraft engines.
700   $aOwen$b A. Karl$01389369
702   $aMattern$b Duane L$g(Duane Loren),
702   $aLe$b Dzu K.
712 02$aLewis Research Center,
712 02$aU.S. Army Research Laboratory,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bOCLCE
801  1$bOCLCE
801  2$bOCLCO
801  2$bOCLCQ
801  2$bGPO
906   $aBOOK
912   $a9910707330203321
996   $aComparisons of rig and engine dynamic events in the compressor of an axi-centrifugal turboshaft engine$93440837
997   $aUNINA