| 研究生: |
謝承甫 Hsieh, Cheng-Fu |
|---|---|
| 論文名稱: |
斜面上帶狀區低溫電漿與震波交互作用之觀察研究 Investigation of shock reflection on a wedged-surface with low temperature Plasmas |
| 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: | 2010 |
| 畢業學年度: | 98 |
| 語文別: | 中文 |
| 論文頁數: | 82 |
| 中文關鍵詞: | 震波 、電漿 、離子風 |
| 外文關鍵詞: | shock, plasmas, ionic wind |
| 相關次數: | 點閱:88 下載:1 |
| 分享至: |
| 查詢本校圖書館目錄 查詢臺灣博碩士論文知識加值系統 勘誤回報 |
本實驗使用視流技術之彩色紋影法與動態壓力測量技巧來探討及比較在有無電漿所產生的離子風在楔形體35度與50度斜面模型上與平面震波交互作用下,其反射震波的結構差異。由於模型角度的差異,在馬赫數為1.35到1.64之間,震波分別在50度模型產生正規反射及35度模型上產生馬赫反射。本研究亦分析了隨著馬赫數的增加,入射震波與反射震波之間的夾角變化與震波強度的變化。由實驗結果的彩色紋影法圖可得知入射震波與反射震波的夾角於無離子風時,隨著入射震波的增強而角度變大,相對之下在有離子風效應下此夾角的變化不明顯。由動態壓力量測結果顯示,在比較有/無電漿產生的離子風效應下的反射壓力脈波,無明顯減弱的趨勢。與前人所使用電漿產生的電暈效應結果相互比較之下,電漿所產生的電暈效應使得震波結構衰減較為顯著,因此發現電暈效應較離子風效應為佳。
The study on a thirty-five degree wedged model and fifty degree wedged model with and without low temperature plasma induced ionic wind under the interaction of a planar shock wave have been done by the color Schlieren flow visualization technique and the dynamic pressure measurement method. It has been shown that with the incident shock Mach number of the range 1.35 to 1.64 there are Mach reflection and regular reflection for wedged models of 35° and 50° respectively. The color Schlieren photographs show that that the angle between incident shock and reflected shock become larger as Mach number increased. These angles do not change much under the influence of the ionic wind. The measured dynamic pressure of reflection shock wave also indicates that its strength is unchanged for models with lower incident Mach number under the influence of ionic wind. Compare with the experimental results with influence of low temperature corona,it has been shown that the reflection shock wave becomes weaker as the incident shock wave pass through the corona. Hence, it is concluded that the corona effect is more efficient than the ionic wind.
[ 1 ] 陳偉仁.“平面震波於楔型體與垂直鱗片模型所產生反射-繞射現象
之探討,”國立成功大學航空太空工程研究所碩士論文,2004.
[ 2 ] V. I. Khorunzhenko,D.V. Roupassov , A. Yu. Starikovskii, “ Hypersonic Flow and Shock Wave structure Control by Low Temperature Non-equilibrium Plasma of Gas Discharge” ,AIAA paper 2002-3569.
[ 3 ] C. Louste, E. Moreau, and G. Touchard, “DC Corona Surface Discharge Along an Insulating Flat Plate in Air: Experimental Results” Annual Report Conference on Electrical insulation and dielectric phenomena, pp.822-826,2002.
[ 4 ] R. Yano, V. Contini, E.Plonjes, P.Palm, S. Merriman, S.Aithal, and I.Adamovich,"Supersonic Nonequilibrium Plasma Wind-Tunnel Measurement of Shock Modification and Flow Visualization," AIAA Journal Vol.38,No.1,October 2000.
[ 5 ] S. Merriman, E.ploenjes,P.Palm,I.V.Adamovich,"shock Wve Control by Nonequilibrium Plasmas in Cold Superosnic Gas Flow,"AIAA Paper 2000-2327,2000.
[ 6 ] S. Merriman, Adam Christian, Rodney Meyer, Brett Kowalczyk, Peter Palm, Igor V.Dmovich,"Studies of Conical Shock Wave Modification by Nonequilibrium RF Discharge Plasma,"AIAA Paper2001-0347,2001.
[ 7 ] Rodney Meyer, Peter Palm, Elke Plonjes, J.William Rich, and Igor V.Adamovich,"The Effect of a Nonequilibrium RF Discharge Plasma on a Conical Shock Wave in a M=2.5 Flow,"AIAA Paper2001-3059,2001.
[ 8 ] V.Bityurin, A.Klimov, S.Leonov, V.brovkin, and Y.Kolesnichenko , “Shock Wave Structure and Velocity at Propagation through Non-homogenous Plasma ,” AIAA Paper 2000-2571,2000.
[ 9 ] Eric Moreau , Christophe Louste , Guillermo Artana , Maxime Forte ,and Gérard Touchard,“Contribution of Plasma Control Technology for Aerodynamic Applications, ”Plasma Process. Polym. 2006, 3, 697–707.
[ 10 ] Richard B.Miles, Sergey O.Macheret, Luigi Martinelli, Robert Murray, Mikhail Shneider, Yu Z. Ionikh, John Kline,and Jon Fox, “Plasma control of shock waves in aerodynamics and sonic boom mitigation, “ AIAA Paper 2001-3062,2001.
[ 11 ]黃冠堯,“楔行體平面上低溫電漿與平面震波交互作用之探討”,國立成功大學航空太空工程研究所碩士論文,2007.
[ 12 ] A. R. Maddox and R. C. Binder, ”A new dimension in Schlieren technique: Flow field analysis using color”, AIAA paper 70-223,1970.
[ 13 ] G. B. Sobeiraj and A. P. Szumowski, “Experimental investigations of an underexpanded jet from a convergent nozzle impinging on cavity,” Journal of Sound and Vibration, Vol.149, No.3, pp.369-375, 1991.
[ 14 ] G. S. Settles, ”Modern developments in flow visualization“,AIAA Journal 24, No.8, pp. 1313-1323., 1986.
[ 15 ] I. I. Glass and G. N. Patterson, ”A theoretical and experimental study of shock-tube flow ”, Journal of Aeronautical Sciences, Vol.22, No.2, pp.73-100, 1955.
[ 16 ] A. G. Gaydon and I. R. Hurle, ”The shock tube in high temperature chemical physics ”, Reinhold Publishing Corp., New York, pp.1-63,1963.
[ 17 ] J. A. Owezarck, ”Fundamentals of gas dynamics “ , International Texbook Company, pp.395-398, 1964.
[ 18 ] R. J. Goldstein, ”Fluid mechanics measurements ”, Second edition,Taylor & Francis publishers, University of Minnesota, pp. 451-474, 1996.
[ 19 ]董家齊,寬任,奇妙的物質第四態-電漿,”成功大學物理學系, ”科學
發展,Vol 354,pp 52-59,2006.