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100   $a20140908j201301    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 14$aThe influence of unsteadiness on the analysis of pressure gain combustion devices /$fDaniel E. Paxson, Tom Kaemming
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJanuary 2013.
215   $a1 online resource (16 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2013-217831
300   $aTitle from title screen (viewed July 9, 2014).
300   $a"January 2013."
300   $a"Prepared for the 51st Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics, Grapevine, Texas, January 7-10, 2013."
300   $a"AIAA-2013-0280."
320   $aIncludes bibliographical references (page 16).
606   $aThermodynamic efficiency$2nasat
606   $aCombustion$2nasat
606   $aPerformance prediction$2nasat
606   $aThermodynamic cycles$2nasat
606   $aSteady flow$2nasat
615  7$aThermodynamic efficiency.
615  7$aCombustion.
615  7$aPerformance prediction.
615  7$aThermodynamic cycles.
615  7$aSteady flow.
700   $aPaxson$b Daniel E.$01386438
702   $aKaemming$b Tom
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704910903321
996   $aThe influence of unsteadiness on the analysis of pressure gain combustion devices$93439579
997   $aUNINA