Muneo Izumikawa

发表

Research on Mixing of Nitrogen Which Simulate Ethylene and Supersonic Flow

Yoshihiro Okuno, Sadatake Tomioka, Ryosuke Hatakeyama, 2014 .

Force Measurements of Fixed-Geometry Scramjet Engines from Mach 4 to 8 Flight Conditions

Syuichi Watanabe, Tetsuo Hiraiwa, Tohru Mitani, 2002 .

Starting Loads in Freejet-type Wind Tunnels.

Takashi Shimura, Sadatake Tomioka, Tetsuo Hiraiwa, 1996 .

Reaction Quenching in Gas Sampling Probes for Scramjet Testing. Part 2: Experimental Validation with a Supersonic Combustor.

Kenji Kudou, Tohru Mitani, Shigeru Sato, 1998 .

Ramjet engine test facility. ( 3 )Engine combution test.

Takashi Shimura, Toshihito Saito, Kouichiro Tani, 1996 .

Evaluation of Air Capture Ratio of Scramjet Inlet by Multi-Point Pressure Measurement

Goro Masuya, Eijiro Kitamura, Noboru Sakuranaka, 2005 .

905 Measurement of Scramjet Engine Drag under M8 Flight Condition

Goro Masuya, Syuichi Watanabe, Tohru Mitani, 2001 .

LOAD OSCILLATIONS CAUSED BY UNSTART OF HYPERSONIC WIND TUNNELS AND ENGINES

Takashi Shimura, Tohru Mitani, Noboru Sakuranaka, 1998 .

Ram and Ejector-Jet Modes Experiments of the Combined Cycle Engine in Mach 4 Flight Conditions

Toshihito Saito, Kouichiro Tani, Muneo Izumikawa, 2008 .

New Injector Geometry for Penetration Enhancement of Perpendicular Jet into Supersonic Flow

Sadatake Tomioka, Akiko Matsuo, Toshinori Kouchi, 2007 .

Vitiation Effects on Scramjet Engine Performance in Mach 6 Flight Conditions

Sadatake Tomioka, Tetsuo Hiraiwa, Kan Kobayashi, 2007 .

Experimental evaluation of mass capture ratio of scramjet inlets

Tetsuo Hiraiwa, Takeshi Kanda, Tohru Mitani, 2004 .

Mach 8 testing of a scramjet engine with ramp compression

Noboru Sakuranaka, Takeshi Kanda, Atsuo Murakami, 2000 .

Performances of a Rocket Chamber for the Combined-cycle Engine at Various Conditions

Sadatake Tomioka, Shuichi Ueda, Toshihito Saito, 2006 .

Gas-sampling Survey from Exhaust Flows in Scramjet Engines at Mach-6 Flight Condition

Sadatake Tomioka, Syuichi Watanabe, Tetsuo Hiraiwa, 2004 .

Comparison of Dual-Mode Combustor Performance with Various Heating Methods

Christopher P. Goyne, Goro Masuya, Sadatake Tomioka, 2011 .

A One-dimensional Analysis of Scramjet Combustion at Mach 6 Flight Conditions

Sadatake Tomioka, Tetsuo Hiraiwa, Kan Kobayashi, 2006 .

Three-Component Force Measurements for Scramjet Engines 2) Effects of External Flow and Boundary Layer Ingestion

Takashi Shimura, Syuichi Watanabe, Tohru Mitani, 2003 .

Penetration of jets injected behind backward-facing step in supersonic stream

Goro Masuya, Sadatake Tomioka, Muneo Izumikawa, 1999 .

Mach 6 Combustion Tests of a Scramjet Engine. Effect of Strut and Isolator.

Kenji Kudo, Shigeru Sato, Takeshi Kanda, 1999 .

Mixing Control by Wall Flush-mount Injectors in Dual-mode Combustor

Sadatake Tomioka, Noboru Sakuranaka, Akiko Matsuo, 2010 .

Experimental study on cellular flame propagation of blend fuels

Tohru Mitani, Takashi Niioka, Muneo Izumikawa, 1988 .

Estimation of Enthalpy Effects in Direct-Connect Dual-Mode Combustor

Christopher P. Goyne, Goro Masuya, Sadatake Tomioka, 2011 .

Supersonic Combustion with Supersonic Injection Through Diamond-Shaped Orifices

Sadatake Tomioka, Akiko Matsuo, Muneo Izumikawa, 2011 .

Combustion Performance of Supersonic Combustor with Stinger-Shaped Fuel Injector

Sadatake Tomioka, Akiko Matsuo, Toshinori Kouchi, 2008 .

Firing-Tests of a Rocket Combustor for Combined Cycle Engine at various conditions

Sadatake Tomioka, Shuichi Ueda, Toshihito Saito, 2005 .