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005 20121026085137.0
035   $a(CKB)5470000002424920
035   $a(OCoLC)814446445
035   $a(EXLCZ)995470000002424920
100   $a20121026d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFoundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines$b[electronic resource] /$fDaniel E. Paxson, Thomas A. Kaemming
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (12 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217443
300   $aTitle from title screen (viewed on Oct. 25, 2012).
300   $a"Prepared for the 50th Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics Nashville, Tennessee, January 9-12, 2012."
300   $a"May 2012."
300   $a"AIAA-2012-770."
320   $aIncludes bibliographical references (page 12).
606   $aGas turbines$2nasat
606   $aCombustion chambers$2nasat
606   $aFlow distribution$2nasat
606   $aPressure ratio$2nasat
606   $aThermodynamics$2nasat
606   $aExtraction$2nasat
606   $aDetonation$2nasat
606   $aCombustion$2nasat
615  7$aGas turbines.
615  7$aCombustion chambers.
615  7$aFlow distribution.
615  7$aPressure ratio.
615  7$aThermodynamics.
615  7$aExtraction.
615  7$aDetonation.
615  7$aCombustion.
700   $aPaxson$b Daniel E$01386438
701   $aKaemming$b Thomas A$01418636
712 02$aNASA Glenn Research Center.
712 12$aAIAA Aerospace Sciences Meeting$d(50th :$f2012 :$eNashville, Tenn.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702122103321
996   $aFoundational performance analyses of pressure gain combustion thermodynamic benefits for gas turbines$93530621
997   $aUNINA