Investigation of Planar Shock Interaction on a Wedged-Surface with Low Temperature Plasma
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 95 === The study on a thirty-five degree wedged model and a fifty degree wedged model with and without low temperature plasma under the interaction of a planar shock wave have been done. The Regular reflection and Mach reflection have been observed on each model wi...
| Main Authors: | , |
|---|---|
| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2007
|
| Online Access: | http://ndltd.ncl.edu.tw/handle/77287370325360685271 |
| Summary: | 碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 95 === The study on a thirty-five degree wedged model and a fifty degree wedged model with and without low temperature plasma under the interaction of a planar shock wave have been done. The Regular reflection and Mach reflection have been observed on each model with Mach number range of 1.35-1.68. As the Mach number increased, the structure of the reflection shock varied. The color Schlieren photograph show that the angle between the incident shock and the reflection shock becomes larger for models under large incident shock Mach number as well as for model with low temperature plasma. The measured dynamic pressure of reflection shock wave indicates that its strength is weaker for models with lower incident Mach number as well as for models with low temperature plasma .
|
|---|