| 研究生: |
許智欽 Hsu, Chih-Chin |
|---|---|
| 論文名稱: |
平面震波與楔形體表面上帶狀區低溫電漿作用之研究 Investigation of Planar Shock on a Wedged Surface with a stripline Low Temperature Plasma |
| 指導教授: |
尤芳忞
Yu, Fan-Ming |
| 學位類別: |
碩士 Master |
| 系所名稱: |
工學院 - 航空太空工程學系 Department of Aeronautics & Astronautics |
| 論文出版年: | 2007 |
| 畢業學年度: | 95 |
| 語文別: | 中文 |
| 論文頁數: | 113 |
| 中文關鍵詞: | 電漿 、震波 |
| 外文關鍵詞: | plasma, shock |
| 相關次數: | 點閱:89 下載:3 |
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入射震波馬赫數1.30~1.69範圍的震波於楔形體表面上低溫電漿作用之定性觀察研究已於國立成功大學航空太空工程所之震波管設備中完成。本實驗使用視流技術之彩色紋影法來擷取震波於斜面35度以及斜面50度楔形體斜面上震波反射的流場結構。平面震波於50度斜面上的反射型態為正規反射,而在35度斜面上之反射型態為馬赫反射。由實驗當中紋影法圖可得知當震波通過低溫電漿時,會造成震波速度減慢、強度減弱,並且形狀改變,反射震波曲率半徑增加,同時配合震波管上壓力感測器所記錄之動態壓力數據,在低溫電漿的作用之下,所測量到反射震波造成的升壓情況較小,且傳遞速度也變慢,由此可確認在低溫電漿的作用之下震波強度的確變弱。
The investigation of the interaction between planar shock wave of Mach number in range of 1.30~1.69 and wedged surface with a stripline of low temperature plasma been done in the shock tube facility of Institute of Aeronautics and Astronautics in National Cheng-Kung University. The flow structure includes shock reflection on the wedges of 50° and 35° were being recorded by color schlieren flow visualization technique. The shock reflection type on the wedges of 50° is regular reflection and the shock reflection type on the wedges of 35° is Mach reflection. The shock wave propagation through low temperature plasma can result in deceleration and weakening of shock wave and both the shape and curvature of shock wave are also being changed. Also, according to the data of measured reflection wave induced pressure pulse, when the low temperature plasma exist, the pressure pulse measured by PT1 is reduced in comparing with the pulse in flow without the plasma and the velocity of reflection shock wave is also slow down.
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