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100   $a20150429j201403    ua             0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aNumerical analysis of a rotating detonation engine in the relative reference frame /$fDaniel E. Paxson
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dMarch 2014.
215   $a1 online resource (16 pages) $ccolor illustrations
225 1 $aNASA/TM ;$v2014-216634
300   $aTitle from title screen (viewed on April 29, 2015).
300   $a"March 2014."
300   $a"Prepared for SciTech 2014 sponsored by the American Institute of Aeronautics and Astronautics, National Harbor, Maryland, January 13-17, 2014."
320   $aIncludes bibliographical references (pages 15-16).
606   $aComputational fluid dynamics$2nasat
606   $aPulse detonation engines$2nasat
606   $aRunge-Kutta method$2nasat
606   $aPropellant combustion$2nasat
606   $aRotary engines$2nasat
615  7$aComputational fluid dynamics.
615  7$aPulse detonation engines.
615  7$aRunge-Kutta method.
615  7$aPropellant combustion.
615  7$aRotary engines.
700   $aPaxson$b Daniel E.$01386438
712 02$aNASA Glenn Research Center,
712 02$aUnited States.$bNational Aeronautics and Space Administration,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910703625903321
996   $aNumerical analysis of a rotating detonation engine in the relative reference frame$93448578
997   $aUNINA