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100   $a20110613d2010      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 12$aA simplified model for detonation based pressure-gain combustors$b[electronic resource] /$fDaniel E. Paxson ; prepared for the 46th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Nashville, Tennessee, July 25-28, 2010
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2010]
215   $a1 online resource (13 pages) $cillustrations, color
225 1 $aNASA/TM ;$v2010-216821
300   $aTitle from title screen (viewed on June 13, 2011).
300   $a"November 2010."
300   $a"AIAA-2010-6717."
320   $aIncludes bibliographical references (pages 12-13).
606   $aDetonation$2nasat
606   $aGas turbines$2nasat
606   $aPulsed jet engines$2nasat
606   $aCombustion chambers$2nasat
606   $aFlow distribution$2nasat
606   $aReliability analysis$2nasat
615  7$aDetonation.
615  7$aGas turbines.
615  7$aPulsed jet engines.
615  7$aCombustion chambers.
615  7$aFlow distribution.
615  7$aReliability analysis.
700   $aPaxson$b Daniel E$01386438
712 02$aNASA Glenn Research Center.
712 12$aAIAA/ASME/SAE/ASEE Joint Propulsion Conference$d(46th :$f2010 :$eNashville, Tenn.)
801  0$bGPO
801  1$bGPO
801  2$bGPO
906   $aBOOK
912   $a9910700371103321
996   $aA simplified model for detonation based pressure-gain combustors$93498662
997   $aUNINA