LEADER 01852nam  2200481   450 
001 9910704025303321
005 20151113160621.0
035   $a(CKB)5470000002437404
035   $a(OCoLC)929073430
035   $a(EXLCZ)995470000002437404
100   $a20151113j201508    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aComparison of numerically simulated and experimentally measured performance of a rotating detonation engine /$fDaniel E. Paxson [and three others]
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dAugust 2015.
215   $a1 online resource (10 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2015-218835
300   $aTitle from title screen (viewed on Nov. 13, 2015).
300   $a"August 2015."
300   $a"Prepared for SciTech 2015 sponsored by the American Institute of Aeronautics and Astronautics, Kissimmee, Florida, January 5-9, 2015."
300   $a"AIAA-2015-1101."
320   $aIncludes bibliographical references (page 10).
606   $aDetonation$2nasat
606   $aComputational fluid dynamics$2nasat
606   $aInlet flow$2nasat
606   $aConvergent-divergent nozzles$2nasat
606   $aPotential flow$2nasat
615  7$aDetonation.
615  7$aComputational fluid dynamics.
615  7$aInlet flow.
615  7$aConvergent-divergent nozzles.
615  7$aPotential flow.
700   $aPaxson$b Daniel E.$01386438
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910704025303321
996   $aComparison of numerically simulated and experimentally measured performance of a rotating detonation engine$93520147
997   $aUNINA