No AccessScramjet Performance Achieved in Engine Tests from M4 to M8 Flight ConditionsTohru Mitani, Sadatake Tomioka, Takeshi Kanda, Nobuo Chinzei and Toshinori KouchiTohru MitaniJapan Aerospace Exploration AgencySearch for more papers by this author, Sadatake TomiokaJapan Aerospace Exploration AgencySearch for more papers by this author, Takeshi KandaJapan Aerospace Exploration AgencySearch for more papers by this author, Nobuo ChinzeiJapan Aerospace Exploration AgencySearch for more papers by this author and Toshinori KouchiTohoku UniversitySearch for more papers by this authorSession: HYTASP-18: Scramjet System DevelopmentPublished Online:26 Jun 2012https://doi.org/10.2514/6.2003-7009SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byRecent advancements in scramjet engine: A review1 Jan 2023Sea-Level Static Tests of Rocket–Ramjet Combined Cycle Engine ModelSadatake Tomioka, Masao Takegoshi, Toshinori Kochi, Kanenori Kato, Toshihito Saito and Kouichiro Tani30 December 2020 | Journal of Propulsion and Power, Vol. 37, No. 3Research on Skin-Friction Drag Reduction by Hydrogen Injection in Supersonic Boundary Layer20 September 2019 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, Vol. 37, No. 3Analysis of Overall Performance of Multi-stage Combustor Scramjet Engine8 June 2019Numerical analysis on the heat transfer of three types of nozzles for the hypersonic long-run wind tunnel30 January 2015 | Science China Technological Sciences, Vol. 58, No. 3Supersonic Combustion Using a Stinger-Shaped Fuel InjectorToshinori Kouchi, Goro Masuya, Kohshi Hirano, Akiko Matsuo and Sadatake Tomioka7 May 2013 | Journal of Propulsion and Power, Vol. 29, No. 3Effect of Local Flow Parameters on Skin-Friction Coefficient in Hypersonic Airbreathing Engines Taira Tsuru , Sadatake Tomioka , Kenji Kudo , Atsuo Murakamo , Kanenori Kao and Hiroyuki Yamasaki 6 September 2013 | Journal of Propulsion and Power, Vol. 28, No. 1Accuracy of Direct Skin-Friction Measurements in High-Enthalpy Supersonic Flows Taira Tsuru , Sadatake Tomioka and Hiroyuki Yamasaki 30 April 2012 | AIAA Journal, Vol. 49, No. 6Supersonic Flow Choking in Engine Wind Tunnels1 Jan 2007 | JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 55, No. 636Suppression of Combustor-Inlet Interaction in a Scramjet Engine under Mach 4 Flight Conditions1 Jan 2007 | TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 49, No. 166Suppression of Combustor-Inlet Interaction in a Scramjet Engine under M4 Flight Conditions1 Jan 2006 | JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, Vol. 54, No. 628Suppression of Combustor-Inlet Interaction in a Scramjet Engine Under M4 Flight ConditionsKan Kobayashi, Sadatake Tomioka, Tetsuo Hiraiwa, Kanenori Kato, Takeshi Kanda and Tohru Mitani26 June 2012 What's Popular 12th AIAA International Space Planes and Hypersonic Systems and Technologies 15 December 2003 - 19 December 2003Norfolk, Virginiahttps://doi.org/10.2514/6.2003-7009 Crossmark TopicsAerodynamicsAerospace SciencesAircraft EnginesCombustion ChambersCombustorsFlow RegimesFluid DynamicsFuel InjectionIgnition SystemsJet EnginesPropulsion and PowerRamjetScramjet KeywordsScramjet EnginesDrag CoefficientDiverging CombustorFriction CoefficientOne Dimensional FlowCombustion EfficiencyCompression RatioDynamic PressureBoundary Layer SeparationFlameholderDigital Topics Hypersonics