Stabilization Time of Wake Behind Hypersonic Capsule
スポンサーリンク
概要
- 論文の詳細を見る
A stabilization time of a wake structure behind a hypersonic vehicle is very important in an experiment on the flow structure by using pulsed facilities of high enthalpy or of high Mach number. However, observations themselves of such wake structure have been very difficult, and therefore, the experimental discussion about the stabilization time itself has also been very difficult. In this study the stabilization time of the wake structure was formulated by using the dimensional analysis and the present experimental results. The experiment was carried out by observing separation points and free shear layers just after capsule models similar to a MESUR pathfinder probe. To visualize the wake structure, one of techniques called the electrical discharge method was utilized. From these investigations it was found that the stabilization time of the wake structure was related to the Reynolds number, the model scale, and the freestream velocity. A hypersonic gun tunnel of Mach 10 was used in this experiment.
- 福山大学の論文
著者
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Nakamura Hiroaki
Fukuyama University
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NISHIO Masatomi
Department of Mechanical System Engineering, Fukuyama University
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SEZAKI Shinji
Fukuyama University
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NAKAMURA Hiroaki
福山大学工学部機械工学科
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NISHIO Masatomi
福山大学工学部機械工学科
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SEZAKI Shinji
福山大学工学部機械工学科
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Nakamura H
Fukuyama University
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Nishio M
Dept. Of Mechanical Engineering Fukuyama University
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Nishio Masatomi
Department Of Mechanical System Engineering Fukuyama University
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Sezaki S
Fukuyama University
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Nisio Masatomi
福山大学工学部機械工学科
関連論文
- Flow Patterns around the MESUR Capsule Traveling at Supersonic/Hypersonic Speeds
- Visualization of Flow Structure Around a Hypersonic Re-entry Capsule Using the Electrical Discharge Method
- 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
- The First Electric Discharge Method for Visualizing Three-Dimensional Shock Shapes Around Hypersonic Vehicles