Influences of Transport Model on Heating Rate of Reentry Vehicles
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概要
- 論文の詳細を見る
We assessed the effect of the models of transport properties for the estimation of the hypersonic reentry heating environment from an engineering point of view. Among the transport properties, we focus on the diffusion of chemical species. For this purpos
- 宇宙航空研究開発機構の論文
著者
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Otsu Hirotaka
Shizuoka University
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Fujita K
Kyoto Univ. Kyoto Jpn
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Abe T
Institute Of Space And Astronautical Science
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Fujita Kazuhisa
Institute of Space and Astronautical Science (ISAS)
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Abe Takashi
Institute of Space and Astronautical Science (ISAS)
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Fujita Kazuhisa
Institute Of Space And Astronautical Science
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Abe Takashi
Institute Of Space And Astronautical Science
関連論文
- Assessment of Forebody and Backbody Radiative Heating Rate of Hypervelocity Reentry Capsule
- Influences of Transport Model on Heating Rate of Reentry Vehicles
- Chemical Nonequilibrium Viscous Shock-Layer Analysis over Ablating Surface of Superorbital Re-Entry Capsule
- Oveview of Research for Prediction of Aerodynamic Heating Environment during a Super-Orbital Reentry Flight of MUSES-C Reentry Capsule
- Low-Temperature Metalorganic Chemical Vapor Deposition of GaAs on Si by Alternate Gas Flow of the Source Materials
- Effect of the Flow Non-uniformity on the Mixing Layer at the Interface of Parallel Supersonic Flows
- NUMERICAL INVESTIGATION OF MAGNETO PLASMA SAIL USING IDEAL MAGNETOHYDRODYNAMIC EQUATIONS
- Experimental Study of Nonequilibrium Phenomena behind Strong Shock Waves Generated in Super-orbital Reentry Flight
- Utilization of Expansion Tube for MUSES-C Reentry Simulation
- Study for Dynamically Unstable Motion of Reentry Capsule
- Development of a Radiation Analysis Code for Hypervelocity Reentry Applications
- Rarefied Aerodynamics of MUSES-C Sample Return Capsule