405 A Study of a Variable Ejector for the Hydrogen Fuel Cell System
スポンサーリンク
概要
- 論文の詳細を見る
- 一般社団法人日本機械学会の論文
- 2005-10-28
著者
-
Setoguchi Toshiaki
Saga Univ. Saga Jpn
-
Setoguchi Toshiaki
Department Of Mechanical Engineering Saga University
-
Setoguchi Toshiaki
Dept.of Mechanical Eng. Saga Univ.
-
Kim Heuy
School Of Mechanical Engineering Andong National University
-
Matsuo Shigeru
Department Of Mechanical Engineering Saga University
-
Matsuo Shigeru
Dept. of Mechanical Engineering, Saga University
-
Matsuo Shigeru
Detp. Of Mechanical Engineering Saga University
-
SETOGUCHI Toshiaki
佐賀大学
関連論文
- 408 A Study of Variable Sonic Ejector Flows
- 405 A Study of a Variable Ejector for the Hydrogen Fuel Cell System
- A NUMERICAL STUDY OF SPIRAL FLOW GENERATED THROUGH AN ANNULAR SLIT(Swirling Flow and Separation)
- A NUMERICAL STUDY OF HETEROGENEOUS CONDENSATION IN AXISYMMETRIC UNDER-EXPANDED JET(Compressible Flow)
- 218 Study on Characteristics of a Variable Critical Nozzle Flow
- A151 Noise Reduction of an Under-expanded Supersonic Jet Using a Rigid Wire Device
- Continuous Wavelet Transform of Pressure Oscillation in Supersonic Cavity Flow
- Passive Control of a Condensation Shock Wave Using a Porous Wall with Cavity
- Experimental Investigation of a Gas Dynamic Thrust Vector Control for Hypersonic Space Planes
- Visualization of Flow Field around a Space Plane Using Smoke Wire Method
- Flow Field around a Space Plane
- Quantitative Cryoimmunogold Electron Microscopic Studies on Induction of Serine: pyruvate Aminotransferase in Rat Liver Mitochondria by Administration of Glucagon
- 411 Starting Process of a Vacuum Ejector-Diffuser System(2)
- 411 Starting Process of a Vacuum Ejector-Diffuser System(1)
- Reduction of Impulsive Noise Caused by Unsteady Compression Wave
- Thrust Vector Control of Non-axisymmetric Nozzles
- Three-dimensional Effects in Overexpanded Nozzle Flows
- Investigation of a Gas Dynamic Thrust Vector Control Using a Semi-empirical Method
- A Study on Characteristics of Under-Expanded Condensing Jet
- CHARACTERISTICS OF MACH DISK AND SONIC LINE OF UNDER-EXPANDED AXISYMMETRIC AIR JET EXHAUST TO REST GAS(Compressible Flow)
- Boundary Layer Bleeding Systems for Hypersonic Airbreathing Propulsion
- Interaction of Supersonic Expansion Flow with Boundary Layer in Unsymmetrical Duct
- CHARACTERISTICS OF OSCILLATION FREQUENCY CAUSED BY SUPERSONIC IMPINGING JET(Impinging Jet)