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Propellant Combustion - From Steady-State Up To Chaos
Novozhilov, B.; Kohno, M.; Shimada, T. unknown 2004 p.1-6
CARS Spectroscopy at High Pressure in a Cryogenic LOX/H~2 Rocket Combustion Chamber
Klimenko, D.; Clauss, W.; Smith, J.; Oschwald, M. unknown 2004 p.7-13
Measuring the Aerodynamic Performance of Scramjet Engines by Multi-Probe-Rakes
Kitamura, E.; Mitani, T.; Izumikawa, M.; Sakuranaka, N.; Masuya, G. unknown 2004 p.14-19
Heat Flux Prediction for Scramjet Engines
Kouchi, T.; Mitani, T.; Hiraiwa, T.; Kodera, M.; Masuya, G. unknown 2004 p.20-26
Relation between Design Parameters of Rocket Nozzles and Phenomena which Generate Severe Side-load
Tomita, T.; Takahashi, M.; Sasaki, M.; Onodera, T.; Tamura, H.; Watanabe, Y.; Furumoto, S. unknown 2004 p.27-32
Experimental Study of Variable Geometry Rectangular Intake for Hypersonic Airbreathing Engine
Kojima, T.; Taguchi, H.; Okai, K. unknown 2004 p.33-38
Cooling Requirement of Combined Cycle Engine in Descending Flight
Kanda, T.; Kudo, K. unknown 2004 p.39-44
Development Status of the ATREX Engine
Ssto, T.; Kobayashi, H.; Taguchi, H.; Kojima, T.; Sawai, S.; Tanatsugu, N.; Kawai, T.; Tomike, J. unknown 2004 p.45-50
Effects of Fluids and Systems on Rotor Vibration of LE-7A Oxygen Turbopump
Shimura, T.; Shimagaki, M.; Watanabe, Y.; Watanabe, M.; Hasegawa, S.; Takata, S. unknown 2004 p.51-56
Eulerian-Lagrangian Approach for Numerical Simulation in Solid Rocket Motors
Sekino, N.; Shimada, T. unknown 2004 p.57-63