An Experimental Study of Shock Wave/Turbulent Boundary Layer Interaction Region Induced by Blunt Protuberance
スポンサーリンク
概要
著者
-
ASO Shigeru
Department of Aeronautics and Astronautics
-
Aso Shigeru
Department Of Aeronautics And Astronautics Faculty Of Engineering Kyushu University
-
MAEKAWA Syozo
Department of Aeronautics and Astronautics,Faculty of Engineering,Kyushu University
-
KARASHIMA Keiichi
Institute of Space and Astronautical Science
-
Karashima K
Nishinippon Inst. Technol. Fukuoka Jpn
-
Maekawa Syozo
Department Of Aeronautics And Astronautics Faculty Of Engineering Kyushu University
-
KARASHIMA Keiichi[et
Institute of Space and Astronautical Science
関連論文
- A Study on Aerodynamic Heating at Jovian Atmospheric Aerocapture. I.
- Study of Cryogenic Mechanical Strength and Fracture Behavior of Adhesives for CFRP Tanks of Reusable Launch Vehicles
- A Study on Unsteady Flow Characteristics and Lateral Force of Conventional Bell-type Nozzle
- A Study on High Temperature Effects in Shock Wave/Boundary Layer Interaction Induced by Compression Corner
- An Experimental Study of Shock Wave/Turbulent Boundary Layer Interaction Region Induced by Blunt Protuberance
- Performance Characteristics of a Free-Piston Shock Tube
- Experimental Studies on Lateral Blowing for the Improvement of Aerodynamic Characteristics of Reusable Launch Vechicles in Subsonic Flow
- Numerical Study on Aerodynamic Heating Reduction by Opposing Jet
- An Experimental Study on Bow Shock Wave/Turbulent Boundary Layer Interaction Region Induced by Blunt Body
- A Study on Improvement of Lift-Drag Characteristics of Transonic Airfoil with Passive Ventilation