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001 9910705619303321
005 20170908152907.0
035   $a(CKB)5470000002452207
035   $a(OCoLC)988393722
035   $a(EXLCZ)995470000002452207
100   $a20170531j200301    ua             0
101 0 $aeng
135   $aurbn|||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$aFuel injector design optimization for an annular scramjet geometry /$fChristopher J. Steffen, Jr
210  1$aCleveland, Ohio :$cNational Aeronautics and Space Administration, Glenn Research Center,$dJanuary 2003.
215   $a1 online resource (15 pages) $cillustrations
225 1 $aNASA/TM ;$v2003-212094
300   $a"January 2003."
300   $a"Prepared for the 41st Aerospace Sciences Meeting and Exhibit sponsored by the American Institute of Aeronautics and Astronautics, Reno, Nevada, January 6-9, 2003."
300   $a"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field" Report documentation page.
300   $a"AIAA-2003-0651."
320   $aIncludes bibliographical references (page 7).
606   $aComputational fluid dynamics$2nasat
606   $aDesign optimization$2nasat
606   $aFuel injection$2nasat
606   $aInjectors$2nasat
606   $aRocket-based combined-cycle engines$2nasat
606   $aSupersonic combustion ramjet engines$2nasat
615  7$aComputational fluid dynamics.
615  7$aDesign optimization.
615  7$aFuel injection.
615  7$aInjectors.
615  7$aRocket-based combined-cycle engines.
615  7$aSupersonic combustion ramjet engines.
700   $aSteffen$b Christopher J.$01386995
712 02$aNASA Glenn Research Center,
801  0$bGPO
801  1$bGPO
906   $aBOOK
912   $a9910705619303321
996   $aFuel injector design optimization for an annular scramjet geometry$93479308
997   $aUNINA