LEADER 01820nam  2200481   450 
001 9910707267903321
005 20160608090639.0
035   $a(CKB)5470000002462827
035   $a(OCoLC)951418247
035   $a(EXLCZ)995470000002462827
100   $a20160608j201604    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aImpact of an exhaust throat on semi-idealized rotating detonation engine performance /$fDaniel E. Paxson
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dApril 2016.
215   $a1 online resource (12 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2016-219076
300   $aTitle from title screen (viewed on June 8, 2016).
300   $a"April 2016."
300   $a"Prepared for the Scitech 2016 sponsored by the American Institute of Aeronautics and Astronautics, San Diego, California, January 4-8, 2016."
300   $a"AIAA-2016-11647."
320   $aIncludes bibliographical references (pages 11-12).
606   $aComputational fluid dynamics$2nasat
606   $aExhaust flow simulation$2nasat
606   $aFuel flow$2nasat
606   $aInviscid flow$2nasat
606   $aPropulsion system performance$2nasat
615  7$aComputational fluid dynamics.
615  7$aExhaust flow simulation.
615  7$aFuel flow.
615  7$aInviscid flow.
615  7$aPropulsion system performance.
700   $aPaxson$b Daniel E.$01386438
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910707267903321
996   $aImpact of an exhaust throat on semi-idealized rotating detonation engine performance$93539463
997   $aUNINA