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100   $a20121203d2012      ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aPerformance impact of deflagration to detonation transition enhancing obstacles$b[electronic resource] /$fDaniel E. Paxson, Frederick Schauer and David Hopper
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$d[2012]
215   $a1 online resource (12 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2012-217629
300   $aTitle from title screen (viewed on Dec. 3, 2012).
300   $a"July 2012."
300   $a"Prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 5-8, 2009."
300   $a"AIAA-2009-502."
320   $aIncludes bibliographical references (page 12).
606   $aPulse detonation engines$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aDeflagration$2nasat
606   $aHeat transfer$2nasat
606   $aAerodynamic drag$2nasat
615  7$aPulse detonation engines.
615  7$aComputational fluid dynamics.
615  7$aDeflagration.
615  7$aHeat transfer.
615  7$aAerodynamic drag.
700   $aPaxson$b Daniel E$01386438
701   $aSchauer$b Frederick F$0263007
701   $aHopper$b David H$g(David Henry),$f1927-$01423225
712 02$aNASA Glenn Research Center.
712 12$aAIAA Aerospace Sciences Meeting$d(47th :$f2009 :$eOrlando, Fla.)
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910702216203321
996   $aPerformance impact of deflagration to detonation transition enhancing obstacles$93550092
997   $aUNINA