LEADER 02019nam  2200529   450 
001 9910705889103321
005 20170815101723.0
035   $a(CKB)5470000002453522
035   $a(OCoLC)994007818
035   $a(EXLCZ)995470000002453522
100   $a20170718j200210    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aMultiple-cycle simulation of a pulse detonation engine ejector /$fS. Yungster, H.D. Perkins
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dOctober 2002.
215   $a1 online resource (10 pages) $cillustration
225 1 $aNASA/TM ;$v2002-211888
300   $a"October 2002."
300   $a"Prepared for the 38th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Indianapolis, Indiana, July 7-10, 2002."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
300   $a"ICOMP-2002-05."
300   $a"AIAA-2002-3630."
320   $aIncludes bibliographical references (pages 4-5).
606   $aDetonable gas mixtures$2nasat
606   $aEjectors$2nasat
606   $aImpulses$2nasat
606   $aMass flow rate$2nasat
606   $aPulse detonation engines$2nasat
606   $aShock waves$2nasat
615  7$aDetonable gas mixtures.
615  7$aEjectors.
615  7$aImpulses.
615  7$aMass flow rate.
615  7$aPulse detonation engines.
615  7$aShock waves.
700   $aYungster$b Shaye$01401113
702   $aPerkins$b Hugh Douglas
712 02$aNASA Glenn Research Center.$bInstitute for Computational Mechanics in Propulsion,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705889103321
996   $aMultiple-cycle simulation of a pulse detonation engine ejector$93469337
997   $aUNINA