| 研究生: |
林榆軒 Lin, Yu-Syuan |
|---|---|
| 論文名稱: |
雷射瑞利散射在乙烯噴注於超音速空氣流場觀察之應用探討 The Application of Laser Rayleigh Scattering for Observation in Supersonic Airflow with Ethylene Injection |
| 指導教授: |
袁曉峰
Yuan, Tony |
| 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: | 2019 |
| 畢業學年度: | 107 |
| 語文別: | 中文 |
| 論文頁數: | 64 |
| 中文關鍵詞: | 超音速燃燒衝壓引擎 、瑞利散射強度觀測 、濃度分布 |
| 外文關鍵詞: | Scramjet engine, Rayleigh scattering, Ethylene |
| 相關次數: | 點閱:83 下載:12 |
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超音速燃燒衝壓引擎由於氣流在進入燃燒室時仍保持高速,讓燃料與空氣保持穩定燃燒成為一個難題。除了加速燃料與空氣混合之外,得知燃料在霧化後於燃燒室內與空氣混合濃度之分布對尋找駐焰位置有很大幫助。本研究欲藉由混合氣體瑞利散射強度與氣體間混合比例有關之特性,進行汽化燃料與空氣混合現象觀測技術的建立。然而航空煤油JP-4為一成分複雜之燃料,故選擇乙烯作為汽化JP-4替代氣體進行研究。
本研究利用校正用觀測艙分別進行氣體混合比例與氣體體積濃度對氣體瑞利散射強度關係觀測,經由實驗結果建立校正用關係曲線。將校正用關係曲線應用於乙烯噴注於超音速流場觀察中,獲得乙烯噴注於超音速流場中與空氣混合之濃度分布。
最後討論此技術應用上如何優化與改進。觀測氣體混合應確定在穩壓狀態下,當氣體壓力變化越大時在氣體混合濃度觀測上的誤差也會越大。觀測儀器收光時間的增加使觀測到的氣體瑞利散射強度增加且可觀測到更多流場細節,代表儀器收光時間能有可調整空間,未來可對此進行改善。
Laser Rayleigh scattering is applied toward measurements of gas visualization, thermometry, and combustion reaction. With the advantages that Rayleigh scattering is elastic and coherent, the signal is easier to detect than Raman scattering and could be enhanced by other factors example: light source. This study discusses the application of laser Rayleigh scattering for measurements in supersonic airflow with hydrocarbon fuel injection. The experimental study is conducted in two different facilities. The correction experiment is conducted in an observation tank and the flow visualization experiment is conducted in in a reflected shock tunnel at National Cheng Kung University. Ethylene become the candidate of the test fuel refer to other studies with similar choice.
The correction of the relationship between gas pressure and signal intensity ensure the signal intensity is proportional to gas pressure. The correction of the relationship between ethylene concentration in air and signal intensity build a correction function for the flow visualization experiment. The measurement about ethylene concentration in mixing gas of ethylene injection in supersonic airflow exist amounts of deviation. Although this method is lack of accuracy about measurement of mixing gas pressure or ethylene concentration, it could measure the structure and forming of ethylene injection in detail. To improve the accuracy of the measurement, block the background noise by moving the pathway of laser light or install more baffle system; Enhance the signal intensity by searching the decent exposure time in ICCD camera.
[1] J. Beloki Perurena, C. O. Asma, R. Theunissen, and O. Chazot, “Experimental Investigation of Liquid Jet Injection into Mach 6 Hypersonic Crossflow”, Experiments in Fluids, Vol.46, No,3, pp403-417, 2009
[2] Pei Kuan Wu, Tzong H. Chen, and Campbell D. Carter, “Injection of Supercritical Ethylene in Nitrogen”, Journal of Propulsion and Power, Vol. 12, No. 4, 1996
[3] Qili Liu, Andrea Passaro, Damiano Baccarella, and Hyungrok, “Ethylene Flame Dynamics and Inlet Unstart in a Model Scramjet”, Journal of Propulsion and Power, Vol. 30, No. 6, 2014
[4] Sergey Leonov, Alec Houpt, Skye Elliott, and Brock Hedlund, “Ethylene Ignition and Flameholding by Electrical Discharge in Supersonic Combustor”, Journal of Propulsion and Power, Vol. 34, No. 2, 2018
[5] Won Keun Chang, Gisu Park, Yuin Jin, and Jongryul Byun, “Shock Impinging Effect on Ethylene Flameholding”, Journal of Propulsion and Power, Vol. 32, No. 5, 2016
[6] A. A. Taha, S. N. Tiwari and T. O. Mohieldin, “Combustion Characteristics of Ethylene in Scramjet Engines”, Journal of Propulsion and Power, Vol. 18, No. 3, 2002
[7] Adela Ben Yakar, and Godfrey Mungal, “Time Evolution and Mixing Characteristics of Hydrogen and Ethylene Transverse Jets in Supersonic Crossflows”, Article in Physics of Fluids, 2006
[8] Alan C. Eckbreth, "Laser Diagnostics for Combustion Temperature and Species", 2nd edition, pp. 13-15, pp. 268-273, 1988
[9] John Strutt, "On the Transmission of Light through an Atmosphere containing Small Particles in Suspension, and on the Origin of the Blue of the Sky," Philosophical Magazine, series 5, vol. 47, pages 375-394, 1899
[10] Ryan THalman, Kyle J. Zarzana, Margaret A. Tolbert, and Rainer Volkamer, “Rayleigh Scattering Cross-Section Measurement of Nitrogen, Argon, Oxygen and Air”, Journal of Quantitative Spectroscopy and Radiative Transfer, 2014
[11] Richard E. Huffman Jr., Martin Boguszko, Gregory S. Eilliott, “Mean and Fluctuating Property Measurements with Filtered Angularly Resolved Rayleigh Scattering”, AIAA Journal, Vol. 49, No. 10, 2011
[12] Stuart L. Seaton, “Gas Density Measurements Using Light Scattering”, Langley Research Center, 1967
[13] William M. Pitts, and Takashi Kashiwagi, “The Application of Laser-induced Rayleigh Light Scattering to the Study of Turbulent Mixing”, National Bureau of Standards, Washington. D. C. 1983
[14] Guanglong Chen, Byunghoon Kim, Byungnam Ahn, and Dong Eon Kim, “Pressure Dependence of Argon Cluster Size for Different Nozzle Geometries”, Journal of Applied Physics, 2009
[15] R. Jeffrey Balla, and Joel L. Everhart, “Rayleigh Scattering Density Measurements, Cluster Theory and Nucleation Calculations at Mach 10”, AIAA Journal, Vol. 50, No. 3, 2012
[16] B. Shirinzadeh, M. E. Hillard, and R. J. Exton, “Condensation Effects on Rayleigh Scattering Measurements in a Supersonic Wind Tunnel”, AIAA Journal, Vol. 29, No. 2, 1991
[17] M. V. Otiigen, J. Kim, and S. Popovic, “Nd: YAG Laser-Based Dual-Line Rayleigh Scattering System”, AIAA Journal, Vol. 35, No. 5, 1997
[18] J. C. Hope and W. C. Honaker “The Application of Laser Rayleigh Scattering to Gas Density Measurements in Hypersonic Helium Flows”, AIAA Paper 79-1086, 1977
[19] Richard G. Seasholtz and Alvin E. Buggele “Study of Injection of Helium Into Supersonic Air Flow Using Rayleigh Scattering”, AIAA Paper 97-0155
[20] Richard G. Seasholtz and Alvin E. Buggele, and Mark F. Reeder “Instantaneous Flow Measurement in a Supersonic Wind Tunnel Using Spectrally Resolved Rayleigh Scattering”, NASA Technical Memorandum 107042, 1995
[21] J. N. Forkey, N. D. Finkelstein, W. R. Lempert, and R. B. Miles, “Demonstration and Characterization of Filtered Rayleigh Scattering for Planar Velocity Measurements”, AIAA Journal, Vol. 34, No. 3, 1996
[22] J. Panda and R.G. Seasholtz,” Velocity and Temperature Measurementin Supersonic Free Jets Using SpectrallyResolved Rayleigh Scattering”, AIAA Paper 99-0296, 2004
[23] Shardanand, and A. D. Prasad Rao, “Absolute Rayleigh Scattering Cross Sections of Gases and Freons of Stratospheric Interest in the Visible and Ultraviolet Regions”, National Aeronautics and Space Administration, 1977
[24] Obraid Faroon, Diane Mandelln, and Hernan Navarro, “Toxicological Profile for Jet Fuels JP-4 and JP-7”, U.S. Department of Health and Human Services, pp. 1-2, pp 67-74, 1995
[25] Hai Zu Zhang, An Song Geng, Yong Qiang Xiong, Jin, and Jin Ping Liu, “Closed-System Programmed-Temperature Pyrolysis on N Octadecane : Implications for the Conversion of Oil to Gas” Geochemical Journal, Vol. 42, pp.403-412, 2008
[26] 張雅筑“氫氣噴注於背階超音速流場之觀察”成功大學航空太空工程學系碩士論文,2013
[27] 梁國邦“氫氣噴注於超音速流場內自燃過程之實驗設計與分析”成功大學航空太空工程學系碩士論文,2012
[28] Harry Ashkenas, and Frederick S. Sherman , “Structure and Utilization of Supersonic Free Jets in Low Density Wind Tunnels”, Rarefid Gas Dyanamics, Vol 2, pp.84-105, 1965
[29] 陳俊岳“反射式震波風洞校驗”成功大學航空太空工程學系碩士論文,2011