Numerical Analysis of the Rarefied Plume from an Arcjet Thruster: Effect of the Nozzle Exit Shape
スポンサーリンク
概要
著者
-
OKAMOTO Hiroyuki
Astro Research Corporation
-
Nishida Michio
Department Of Aemonautical Engineering Kyushu University
関連論文
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- Application of a 20kW Arc-Heated Wind Tunnel to Evaluation Tests of Wall Catalysis
- DSMC-PIC Analysis of a Plume from MUSES-C Ion Engines
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- Freejets of Rotationally Relaxing Diatomic Gases
- Computational and Experimental Studies of Unsteady Viscous Nozzle Flows
- Experimental and Numerical Studies of a Low-Power N_2 Arcjet Thruster
- Viscous Shock Layer Studies of a Super Orbital Reentry Capsule Using a Multi Vibrational Temperature Model
- A Thermochemical Nonequilibrium Flow around a Super Orbital Reentry Capsule with Ablation
- Numerical Studies of Oblique Shock Reflection in Steady Two-Dimensional Flows
- Numerical Analysis of a Radiation-Cooled Micro Arcjet Thruster
- Ablation Studies for a Super-Orbital Reentry Capsule Using a Three-Temperature Model
- DSMC Simulation of Parallel, Oblique and Normal Free Jet Impingements on a Flat Plate
- Fundamental Research of Planetary Aerobrake Technology
- Studies on Stagnation Flow of a Partially Ionized Gas
- Numerical Analysis of Thermochemical Nonequilibrium Flows Using a Diagonal Lower-Upper Implicit Scheme
- Flow Visualization of Sonic Jets Exhausting Counter to a Supersonic Free Stream Using Laser Induced Fluorescence Method
- Density Measurements of a Free Jet by a Laser Differential Interferometer
- VSL Analysis of the Flow Field over a Super Orbital Reentry Capsule
- Numerical Simulation of a Nitorogen Arcjet Thruster
- Numerical Analysis of the Rarefied Plume from an Arcjet Thruster: Effect of the Nozzle Exit Shape
- Focusing shock waves generated by an accelerating projectile
- Numerical Analysis of Gas-Solid Two-Phase Nonequilibrium Nozzle Flows
- DSMC-PIC Analysis of a Plume from MUSES-C Ion Engines