Visualization Method of Hypersonic Capsule Wake Using Electrical Discharge
スポンサーリンク
概要
- 論文の詳細を見る
The visualization of the wake structure behind hypersonic vehicle was carried out using a new method for the experiment a Mach 10 pulsed gun tunnel. In the experiment the separation point, free shear layer, and rear stagnation point were visualized. The experimental results were compared with numerical ones. From the result the experimental separation point and free shear layer agreed considerably well with numerically calculated one.
- 福山大学の論文
著者
-
NAKAMURA Hiroaki
福山大学工学部機械工学科
-
NISHIO Masatomi
福山大学工学部機械工学科
-
SEZAKI Shinji
福山大学工学部機械工学科
-
NAI Hiroaki
福山大学工学部機械工学科
関連論文
- FEM Simulation of Hypersonic Reaetivc Flows Around Re-entry Capsule
- Stabilization Time of Wake Behind Hypersonic Capsule
- Study on Shock-Wave/Boundary-Layer Interaction in Hypersonic Flow
- Flowfield Around MUSES-C Superorbital Re-entry Capsule
- Flowfield around Hypersonic MESUR Capsule
- Numerical Calculation around Hypersonic/Supersonic Capsule
- Investigation of Flowfield around Hypersonic Space Plane
- Visualization Method of Hypersonic Capsule Wake Using Electrical Discharge
- Method for Visualizing Gas Temperature Field Around Hypersonic Vehicles
- The Second Electric Discharge Method for Visualizing Three Dimensional Shock Shapes