An Experimental Study on the Boundary Layer Transition due to Gas Injection from Capsule-shape Body Surface
スポンサーリンク
概要
- 論文の詳細を見る
In order to study the onset of the ablation gas-induced boundary layer transition during the reentry phase, heat flux measurement through infrared thermography has been conducted on the capsule-shape body with gas injection from the porous material surfac
- 宇宙航空研究開発機構の論文
著者
-
Nonaka Satoshi
Institute Of Space And Astronautical Science Japan Aerospace Exploration Agency
-
Nonaka Satoshi
Institute Of Space And Astionautical Science Japan Aerospace Exploration Agency
-
OGAWA Hiroyuki
Institute of Molecular and Cellular Biosciences, The University of Tokyo
-
INATANI Yoshifumi
Institute of Space and Astionautical Science, Japan Aerospace Exploration Agency
-
Yamada Tetsuya
Institute of Space and Astronautical Science (ISAS)
-
Nonaka Satoshi
Institute Of Space And Astronautical Science
-
Nakakita Kazuyuki
National Aerospace Laboratory
-
Yamazaki Takashi
National Aerospace Laboratory
-
Yamada Tetsuya
Institute Of Space And Astronautical Science
-
Nakakita K
National Aerospace Laboratory
-
Inatani Yoshifumi
Institute Of Space And Astionautical Science Japan Aerospace Exploration Agency
-
Ogawa Hiroyuki
Institute Of Space And Astronautical Science
-
Ogawa Hiroyuki
Institute Of Molecular And Cellular Biosciences The University Of Tokyo
関連論文
- Phylogenetic positions of rust fungi parasitic on ferns: Evidence from 18S rDNA sequence analysis
- Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM(CIP)
- Thermal Responses of Ablator for Reentry Capsules with Superorbital Velocity
- An Experimental Study on the Boundary Layer Transition due to Gas Injection from Capsule-shape Body Surface
- Design Overview of an Asteroid Sample Return Capsule
- System Description and Reentry Operation Scenario of MUSES-C Reentry Capsule
- Attitude Motion and Aerodynamic Characteristics of MUSES-C Reentry Capsule
- A Unique Single Stage Parachute System and Qualification by Balloon Drop Tests
- Thermal Protection System of the Reentry Capsule with Superorbital Velocity
- Deep Space Flight of Microwave Discharge Ion Engines onboard Hayabusa
- Measurement of Hypersonic Flow Fields around a Sidewall Compression Scramjet Inlet Using Shock Tunnel Experiments
- The Aerodynamic Data Base for Asteroid Sample Return Capsule
- Rarefied Aerodynamics of MUSES-C Sample Return Capsule
- Nonequilibrium Temperatures Measurement in an Arc-Heated Airflow by the Optical Diagnostic Method
- JAPANESE ROCKET SOCIETY'S ROCKET SYMPOSIA 1995-2001 : With an Overview of Japanese Rocket Society's Space Tourism Study
- Arc Heating Facility and Test Technique for Planetary Entry Missions
- FLIGHT DEMONSTRATION AND A CONCEPT FOR READINESS OF FULLY REUSABLE ROCKET VEHICLES
- Investigation of Aerodynamic Forces on Scramjet Inlets Using Shock Tunnel Tests