No AccessA comparison of scramjet engine performances of various cyclesTAKESHI KANDA, GORO MASUYA, YOSHIO WAKAMATSU, NOBUO CHINZEI and AKIO KANMURITAKESHI KANDANational Aerospace Laboratory, Kakuda, JapanSearch for more papers by this author, GORO MASUYANational Aerospace Laboratory, Kakuda, JapanSearch for more papers by this author, YOSHIO WAKAMATSUNational Aerospace Laboratory, Kakuda, JapanSearch for more papers by this author, NOBUO CHINZEINational Aerospace Laboratory, Kakuda, JapanSearch for more papers by this author and AKIO KANMURINational Aerospace Laboratory, Kakuda, JapanSearch for more papers by this authorPublished Online:17 Aug 2012https://doi.org/10.2514/6.1989-2676SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byA novel liquid metal MHD enhanced Closed-Brayton-Cycle power generation system for hypersonic vehicles: Thermodynamic analysis and performance evaluation with finite cold source1 Sep 2022 | Energy Conversion and Management, Vol. 268Experimental and theoretical investigation of power generation scheme driven by thermal cracked gaseous hydrocarbon fuel for hypersonic vehicle1 Jun 2018 | Energy Conversion and Management, Vol. 165Comparison Analysis between Expander Cycle and Recooling Cycle for a Scramjet1 Jul 2012 | Journal of Aerospace Engineering, Vol. 25, No. 3 What's Popular 25th Joint Propulsion Conference 12 July 1989 - 16 July 1989Monterey,CA,U.S.A.https://doi.org/10.2514/6.1989-2676 Crossmark TopicsAircraft EnginesCombustion ChambersCombustorsCoolantCooling TechnologyFuel InjectionHeat TransferIgnition SystemsJet EnginesNozzlesPropellantPropulsion and PowerScramjetThermophysics and Heat TransferTurbinesTurbomachinery KeywordsScramjet EnginesMach NumbersDynamic PressureFuel InjectionCombustorsCombustion ProductsClosed LoopStaged Combustion CyclePropellantCoolantDigital Topics Joint Propulsion