| 研究生: |
陳孟巧 Chen, Meng-Chiao |
|---|---|
| 論文名稱: |
探討圓柱在臨界區之流場轉換現象 Investigations of Transition Phenomenon of the Flow around a Circular Cylinder in the Critical Regime |
| 指導教授: |
苗君易
Miau, Jiun-Jih |
| 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: | 2011 |
| 畢業學年度: | 99 |
| 語文別: | 中文 |
| 論文頁數: | 86 |
| 中文關鍵詞: | 圓柱流場 、臨界區 、分離泡 、希爾伯特-黃轉換 、熱絲感測組 |
| 外文關鍵詞: | circular cylinder, critical regime, separation bubble, Hilbert-Huang transformation, MEMS thermal tuft sensor |
| 相關次數: | 點閱:101 下載:3 |
| 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 |
本研究以實驗方式來探討圓柱表面流場於雷諾數為1.53×105~3.92×105間之流場轉換現象。實驗利用基部壓力隨雷諾數變化,再配合圓柱左右兩側θ=±90˚之擾動壓力訊號來判斷圓柱從預臨界區到單分離泡區至雙分離泡區的分界。研究內容主要利用基部壓力係數及圓柱左右兩側θ=±80˚、±90˚之壓力係數搭配熱線探針(Hot-wire)來觀察流場之瞬時訊號。由於單分離泡會造成尾流偏移,吾人同時在單分離泡出現時,置一熱線探針於尾流區,固定X軸及Z軸位置,移動Y軸於一範圍內量測尾流訊號,並同時也量測預臨界區及雙分離泡區做比較。
另外,同時使用熱絲觀念(Thermal tuft)在圓柱θ=±92˚量測,經由訊號可判定此角度下流場為順流抑或是逆流,進而判定流體是否已在圓柱表面分離,並由即時訊號得到流場當下流況。接著再於單分離泡及雙分離泡出現時,轉動圓柱改變熱絲感測器(MEMS sensors)之角度,期望藉由訊號顯示之順逆流找出流動分離及回覆再接觸現象發生之位置。
至於瞬時頻率之分析,藉由希爾伯特-黃轉換進行數據處理,得到瞬時溢放頻率及能量大小,此方法貢獻了快速傅立葉轉換無法得到之瞬時頻率。
This study aims to investigate the transition phenomenon of flow around a circular cylinder in the critical regime at Reynolds numbers between 1.53×105~3.92×105.The base-pressure coefficients and the root-mean-square of the pressure coefficients on two sides of a cylinder were used to determine the pre-critical regime, the one bubble regime, and the two bubble regime. The main purpose of this study was to analyze the instantaneous signals which were measured by the pressure transducers on the cylinder surface and a hot-wire in the wake region. Because the wake flow was shifted in lateral direction while one bubble developed on the cylinder surface, a hot-wire probe was employed to measure the wake velocity profiles at X/D=2 and Z/D=0. Meanwhile, the wake velocity profiles were obtained with respect to the pre-critical regime and the two bubble regime for comparative study.
Besides, self-made MEMS thermal films sensors located at θ=±92˚ were carried out . A thermal tuft method was used to determine the flow direction at the position measured. Moreover, in order to determine the position of separation point and reattachment point, the cylinder was rotated while the bubble appeared stably.
The instantaneous behavior of vortex shedding was studied by analyzing the measured data with Hilbert-Huang transformation. This method offers instantaneous information that fast Fourier transformation can not provide.
[1] Miau, J. J., Chou, J. H., Cheng, C. M., Chu, C. R., Woo, K. C., Ren, S. K., Chen, Z. L., Hu, C. C. & Chen, J. L., "Design aspects of the ABRI wind tunnel," The International Wind Engineering Symposium, Taipei County, Taiwan, 2003.
[2] 高義明, "內政部建研所環境風洞校驗及二維鈍形體空氣動力流場實驗研究," 成功大學航太所碩士論文, 2005.
[3] Niemann, H. J. and Hölscher, N., "A review of recent experiments on the flow past circular cylinders," Journal of Wind Engineering and Industrial Aerodynamics, vol. 33, pp. 197-209, 1990.
[4] Roshko, A., "Experiments on the flow past a circular cylinder at very high Reynolds number," Journal of Fluid Mechanics, vol. 10, pp. 345-356, 1961.
[5] Achenbach, E., "Distribution of local pressure and skin friction around a circular cylinder in cross-flow up to Re = 5×106," Journal of Fluid Mechanics, vol. 34, pp. 625-639, 1968.
[6] Bearman, P. W., "On vortex shedding from a circular cylinder in the critical Reynolds number," Journal of Fluid Mechanics, vol. 37, pp. 577-585, 1969.
[7] Achenbach, E., "Influence of surface roughness on the cross-flow around a circular cylinder," Journal of Fluid Mechanics, vol. 46, pp. 321-335, 1971.
[8] Zdravkovich, M. M., "Flow around circular cylinders," Vol.1: Fundamentals, Oxford University Press, 1997.
[9] Zdravkovich, M. M., "Conceptual overview of laminar and turbulent flows past smooth and rough circular cylinders," Journal of Wind Engineering and Industrial Aerodynamics, vol. 33, pp. 53-62, 1990.
[10] Schewe, G., "Reynolds-number effects in flow around more-or-less bluff bodies," Journal of Wind Engineering and Industrial Aerodynamics, vol. 89, pp. 1267-1289, 2001.
[11] Noack, B. R., "On the flow around a circular cylinder.Part 1 laminar and regime," 1999.
[12] Noack, B. R., "On the flow around a circular cylinder.Part 2 turbulent regime," 1999.
[13] Szepessy, S. and Bearman, P. W., "Aspect ratio and end plate effects on vortex shedding from a circular cylinder," Journal of Fluid Mechanics, vol. 234, pp. 191-217, 1992.
[14] Uematsu, Y. and Yamada, M., "Effects of aspect ratio and surface roughness on the time-averaged aerodynamic forces on cantilevered circular cylinders at high Reynolds numbers," 1995.
[15] Achenbach, E. and Heinecke, E., "On vortex shedding from smooth and rough cylinders in the range of Reynolds numbers 6×103 to 5×105," Journal of Fluid Mechanics, vol. 109, pp. 239-251, 1981.
[16] Batham, J. P., "Pressure distributions on circular cylinders at critical Reynolds numbers," Journal of Fluid Mechanics, vol. 57, pp. 209-228, 1973.
[17] Güven, O., Farell, C., and Patel, V. C., "Surface-roughness effects on the mean flow past circular cylinders," Journal of Fluid Mechanics, vol. 98, pp. 673-701, 1980.
[18] Adachi, T., "Effects of surface roughness on the universal Strouhal number over the wide Reynolds number range," Journal of Wind Engineering and Industrial Aerodynamics, vol. 69-71, pp. 399-412, 1997.
[19] "Mean forces, pressures and flow field velocities for circular cylindrical structures : single cylinder with two-dimensional flow," ESDU, 1980.
[20] Kiya, M., Suzuki, Y., Arie, M., and Hagino, M., "A contribution to the free-stream turbulence effect on the flow past a circular cylinder," Journal of Fluid Mechanics, vol. 115, pp. 151-164, 1982.
[21] Farell, C. and Blessmann, J., "On critical flow around smooth circular cylinders," Journal of Fluid Mechanics, vol. 136, pp. 375-391, 1983.
[22] Schewe, G., "On the force fluctuations acting on a circular cylinder in crossflow from subcritical up to transcritical Reynolds numbers," Journal of Fluid Mechanics, vol. 133, pp. 265-285, 1983.
[23] Zan, S. J. and Matsuda, K., "Steady and unsteady loading on a roughened circular cylinder at Reynolds numbers up to 900,000," Journal of Wind Engineering and Industrial Aerodynamics, vol. 90, pp. 567-581, 2002.
[24] Humphreys, J. S., "On a circular cylinder in a steady wind at transition Reynolds numbers," Journal of Fluid Mechanics, vol. 9, pp. 603-612, 1960.
[25] Korotkin, A. I., "The three dimensionality of the flow transverse to a circular cylinder," Fluid Mechanics, vol. Vol.5, 1976.
[26] Miau, J., Tsai, H., Lin, Y., Tu, J., Fang, C., and Chen, M., "Experiment on smooth, circular cylinders in cross-flow in the critical Reynolds number regime," Experiments in Fluids, pp. 1-19, 2011.
[27] Ying-Ju Lin, J.-J. M., Jung-Kuo Tu and Hsing-Wen Tsai, "Non-Stationary, Three-Dimensional Aspects of Flow Around a Circular Cylinder at Critical Reynolds Numbers," AIAA JOURNAL, 2011.
[28] Schlichting, H., "Boundary-Layer Theory," McGraw-Hill, New York. 7th ed., 1979.
[29] Schewe, G., "Sensitivity of transition phenomena to small perturbations in flow round a circular cylinder," Journal of Fluid Mechanics, vol. 172, pp. 33-46, 1986.
[30] Almosnino, D., Mcalister, K. W., and "Water tunnel study of transition flow around circular cylinders," NASA, 1984.
[31] Nikitas, N., Macdonald, J. H. G., Andersen, T. L., Jakobsen, J. B., Savage, M. G., and McAuliffe, B. R., "Wind tunnel testing of an inclined aeroelastic cable model Pressure and motion characteristics, Part I," 2009.
[32] Nikitas, N., Macdonald, J. H. G., Andersen, T. L., Jakobsen, J. B., Savage, M. G., and McAuliffe, B. R., "Wind tunnel testing of an inclined aeroelastic cable model Pressure and motion characteristics, Part II," 2009.
[33] Higuchi, H., Kim, H. J., and Farell, C., "On flow separation and reattachment around a circular cylinder at critical Reynolds numbers," Journal of Fluid Mechanics, vol. 200, pp. 149-171, 1989.
[34] von Papen, T., Steffes, H., Ngo, H. D., and Obermeier, E., "A micro surface fence probe for the application in flow reversal areas," Sensors and Actuators A: Physical, vol. 97-98, pp. 264-270, 2002.
[35] Lee, T., "Investigation of unsteady boundary layer developed on a rotationally oscillating circular cylinde," AIAA JOURNAL, vol. 37, 1999.
[36] Liu, W. P. and Brodie, G. H., "A demonstration of MEMS-based active turbulence transitioning," International Journal of Heat and Fluid Flow, vol. 21, pp. 297-303, 2000.
[37] Fukang, J., Yu-Chong, T., Walsh, K., Tsao, T., Gwo-Bin, L., and Chih-Ming, H., "A flexible MEMS technology and its first application to shear stress sensor skin," in Micro Electro Mechanical Systems, 1997. MEMS '97, Proceedings, IEEE., Tenth Annual International Workshop on, 1997, pp. 465-470.
[38] 杜榮國, "MEMS熱膜感測器設計製造及應用於探討非定常流分離現象," 成功大學航太所碩士論文, 2003.
[39] Tu, J. K., Miau J. J., Wang Y. J. , Lee G. B. and Lin C. , "Studying three-dimensionality of vortex shedding behind a circular cylinder with MEMS sensors, accepted by Journal of Mechanics," 2006.
[40] 蔡星汶, "圓柱表面流場在臨界區之空氣動力實驗研究," 成功大學航太所碩士論文, 2006.
[41] Huang, N. E., Shen, Z., Long, S. R., Wu, M. C., Shih, H. H., Zheng, Q., Yen, N. C., Tung, C. C., and Liu, H. H., "The empirical mode decomposition and the Hilbert spectrum for nonlinear and non-stationary time series analysis," Proceedings of The Royal Society A: Mathematical, Physical and Engineering Sciences, vol. 454, pp. 903-995, 1998.
[42] Wu, Z. and Huang, N. E., "Ensemble Empirical Mode Decomposition: a Noise-Assisted Data Analysis Method," Advances in Adaptive Data Analysis, vol. 1, pp. 1-41, 2009.
[43] Roshko, A., "Perspectives on bluff body aerodynamics," Journal of Wind Engineering and Industrial Aerodynamics, vol. 49, pp. 79-100, 1993.
[44] Nishimura, H. and Taniike, Y., "Aerodynamic characteristics of fluctuating forces on a circular cylinder," Journal of Wind Engineering and Industrial Aerodynamics, vol. 89, pp. 713-723, 2001.
[45] 林映如, "臨界圓柱體流場之非定常三維特性探討," 成功大學航太所碩士論文, 2007.
[46] Fujita, K., Ikegami, Y., Kobayashi, K., and Ohashi, M., "experimental studies on fluctuating lift force on a single circular cylinder at high Reynolds numbers (in English)," Japan Journal Wind Engineering, pp. 73~82, 1998.
[47] Zan, S. J., "Experiments on circular cylinders in crossflow at Reynolds numbers up to 7 million," Journal of Wind Engineering and Industrial Aerodynamics, vol. 96, pp. 880-886, 2007.