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空氣動力學

 期刊:

  1. Chung, K., 2006, ``Investigation on Compressible Ramp Flows,’’ Journal of Aeronautics, Astronautics and Aviation, Series A, Vol. 38, No. 3, pp. 167-172.

  2. 劉怡眉、林怡君、張克勤、鍾光民, 2006, ``降低太陽能熱水器風阻之探討與測試,’’ Journal of Aeronautics, Astronautics and Aviation, Series B, Vol. 38, No. 1, pp. 49-54.

  3. Chung, K., 2004, ``Unsteadiness of Transonic Convex-Corner Flows,’’ Experiments in Fluids, Vol. 37, No. 6, pp. 917-922.

  4. Zinoviev, V., Lebiga, V., Chung, K., and Miau, J., 2004, ``Using Hilbert Analysis in Hot-Wire Measurements in Compressible Subsonic Flows,’’ Transactions of the Aeronautical and Astronautical Society of the Republic of China, Vol. 36, No. 2, pp. 115-124.

  5. Chung, K., 2004, ``Aerodynamic Characteristics of Deflected Surface in Compressible Flows’’, Journal of Aircraft, Vol. 41, No. 2, pp. 415-418.

  6. Chung, K., 2003, ``Transonic Cavity-Convex Corner Interactions,’’ Journal of Aircraft, Vol. 40, No.6, pp. 1131-1136.

  7. Chung, K., 2003, ``Characteristics of Compressible Concave-Corner Flows,’’ Journal of Aircraft, Vol. 40, No.4, pp. 797-799.

  8. Chung, K., 2003, ``Characteristics of Compressible Rectangular Cavity Flows,’’ Journal of Aircraft, Vol. 40, No.1, pp. 137-142.

  9. Chung, K., 2003, ``Transonic Cavity-Convex Corner Interactions,’’ to be published in Journal of Aircraft.

  10. Chung, K., 2002, ``Investigation on Transonic Convex-Corner Flows,’’ Journal of Aircraft, Vol. 39, No. 6, pp. 1014-1018.

  11. Chung, K., 2002, ``Cavity Effect on Transonic Convex Corner Flows,’’ Shock Waves, An International Journal, Vol. 12, No. 3, pp. 177-180.

  12. 周大維, 苗君易, 鍾光民, 周榮華, 2002, ``透氣參數法修正穿音速風洞二維洞壁干擾效應,’’ 中國航空太空學會學刊, 第34卷, 第2期, 143-151頁.

  13. Chung, K., 2002, ``Geometry Effect on Compressible Rectangular Cavity Flows,’’ Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 45, No. 147, pp. 28-34.

  14. 鍾光民, 2001, ``開放式凹槽對穿音速凸角流影響之研究,’’中國航空太空學會學刊, 第33卷, 第4期, 303-308頁.

  15. Chung, K., 2001, `` Static Pressure Measurements of Compressible Rectangular Cavity Flows,’’ Journal of Aeronautical Technology, Vol. 3, No. 2, pp. 1-13.

  16. Chung, K., 2001, ``Three-Dimensional Effect on Transonic Rectangular Cavity Flows,’’ Experiments in Fluids, Vol. 30, No.5, pp.531-536 (SCI, EI).

  17. Chung, K., 2000, ``Transition of Subsonic and Transonic Expansion-Corner Flows,’’ Journal of Aircraft, Vol. 37, No. 6, pp. 1079-1082.

  18. Chung, K., 2001, ``Investigation on Turbulent Expansion-Corner Flows with Shock Impingement,’’ Transactions ASME Journal of Fluids Engineering, Vol. 123, Issue 1, pp. 139-144.

  19.  Chung, K., 2000, ``Characteristics of Transonic Rectangular Cavity Flows,’’ Journal of Aircraft, Vol. 37, No. 3, pp. 463-468 (SCI, EI).

  20. 張國治, 苗君易, 鍾光民, 周榮華, 2000, ``穿音速機翼之表面視流觀察研究,’’ 中國航空太空學會學刊, 第32卷, 第2期, 137-146頁.

  21. Chung, K., 1999, ``Pressure Fluctuations in Rectangular Cavity Flows,’’ The Chinese Journal of Mechanics, Vol. 15, No. 3, pp. 97-102

  22. Chung, K., 1998, ``Wall Pressure Fluctuations of a Low-Supersonic Expansion Corner Flow,’’ Transactions of the Aeronautical and Astronautical Society of the Republic of China, Vol. 30, No. 3, pp.231-236.

  23. Chung, K., 1998, ``Interaction Region of Turbulent Expansion-Corner Flows,’’ AIAA Journal, Vol. 36, No. 6, pp. 1115-1116

研討會論文:

  1. Zinovyev, V.N., Lebiga, V.A., Miau, J.J., Chung, K.M., Hu, C.C. and Tu, I.K., 2006, ``Experimental Investigation of Flow Fluctuations around the Cylinder in Subsonic Flows with the Help of Hilbert Transform and EMD Technique,’’ 2006 Taiwan-Russia Symposium on Numerical and Experimental Modeling of Microprocesses and Its Application in Continuum Mechanics, November 28-29, Tainan, Taiwan.

  2. Chen, Y.S., Miau, J.J. and Chung, K., 2006, ``The Application of MEMS Thermal-Film Sensor Arrays on the Measurement of Transonic Models,’’ 2006 Taiwan-Russia Symposium on Numerical and Experimental Modeling of Microprocesses and Its Application in Continuum Mechanics, November 28-29, Tainan, Taiwan.

  3. Chung, K., 2006, ``Surface Pressure Measurements of Compressible Corner Flows,’’ 5th Indonesia-Taiwan Workshop on Aeronautical Science, Technology and Industry, Tainan, November 13-14.

  4. Chung, K., Chang, K. and Cheng, J., 2006, ``Guiding Plates on Wind Uplift of a Solar Collector Model,’’ International Symposium on Advanced Fluid/Solid Science and Technology in Experimental Mechanics, September 11-14, Sapporo, Japan

  5. Chung, K., Chang, K., Liu, Y. and Lin, Y., 2006, ``Reduction of Wind Load on a Solar Collector Model,’’ 17th International Symposium on Transport Phenomena, September 4-8, Toyama, Japan.

  6. 鍾光民, 2006, ``上游噴流對穿音速凸角流的效應,’’ 第五屆海峽兩岸航空太空學術研討會， 淡江大學，3月14-15日.

  7.  劉怡眉、林怡君、張克勤、鍾光民, 2005, ``低風阻太陽能熱水器之設計測試,’’ 2005中國航太學會/民航學會聯合學術研討會, 12月10日.

  8. Chung, K. and Liao, T., 2005, ``Shock Induced Separation of Transonic Convex-Corner Flows,’’ 2005 Joint Conference of Aeronautical and Astronautical Society/Chinese Civil Aviation Society, December 10.

  9. Chung, K., 2005, ``Transonic Convex Corner Flows,’’ Workshop of Institute of Theoretical and Applied Mechanics (Russia) and Aerospace Science and Technology Research Center (Taiwan), Oct. 24-28, 2005.

  10. Jeng, Y. and Chung, K., 2005, ``The Application of a Modified Morlet Transform to Shock and/or Vortex Flow Field,’’ Second Asia-Pacific Workshop on Shock and Vortex Interactions, June 25-29, DunHuang, GanSu, China.

  11. Chung, K. and Li, C., 2005, ``Upstream Blowing jet on Transonic Convex-Corner Flows,’’ 43th AIAA Aerospace Science Meeting and Exhibit, Reno, USA, Jan 10-12, AIAA Paper 2005-0644.

  12. Chung, K., 2004, ``Aerodynamic Characteristics of Deflected Surface in Compressible Flows,’’ 2004 International Congress of Aeronautical Society, Yokohama Japan, ICAS 2004-3.6.2, August 29-September 3.

  13. Chung, K., 2004, ``Transonic Convex-Corner Flow with Upstream Blowing,’’ 2004 Regional Conference on Aeronautical Science, Technology and Industry, Bandung Indonesia, May 18-19.

  14. Liu, J., and Chung, K., 2003, ``A Preliminary Experimental and Theoretical Study on properties of Induced Oblique Waves of Weak Supersonically Flying Straight Wedges,’’ 27th National Conference in Theoretical and Applied Mechanics, National Cheng Kung University, Dec. 12-13.

  15. Chung, K., 2003, ``Transonic Convex Corner Flows with an Upstream Cavity,’ 27th National Conference in Theoretical and Applied Mechanics, National Cheng Kung University, Dec. 12-13.

  16. Chung, K., 2003, ``Cavity Effect on Transonic Convex-Corner Flows,’’ 5th International Workshop on Shock/Vortex Interaction,’’ October 27-31, Grand Hotel, Kaohsiung, Taiwan.

  17. Chung, K., Miau, J., Lee, J., and Zharkova, G., 2002, ``Application of Liquid Crystal for Flow Visualization in Wind Tunnel Testing,’’ International Symposium in Experimental Mechanics, December 28-30, Grand Hotel, Taipei, Taiwan.

  18. 李佳峰, 苗君易, 鍾光民, 黃守仁, 劉瑞祥, 鍾武錕, 周榮華, 2002, ``在成大發展壓力感測塗料量測技術,’’ 笫26屆全國應用力學研討會, 虎尾技術學院.

  19. Chung, K., 2002, ``Investigation on Subsonic Ramp Flows,’’ Proc. 3rd Indonesia-Taiwan Workshop on Science, Technology and Industry of Aeronautics, December 16, Bandung, Indonesia.

  20. Chung, K., 2002, ``An Experimental Study of Compressible Concave Corner Flows,'' 2002 International Conference on the Methods of Aerophysics Research, July 1-5, 2002, Novosibirsk, Russia.

  21. Miau, J., Lin, C., Chung, K., Chou, J. and Liu, J., 2002, `` Normal and Side Forces Amplification by Lateral Jet Issued from An Ogive Cylinder,’’ 2002 International Conference on the Methods of Aerophysics Research, July 1-5, 2002, Novosibirsk, Russia.

  22. 林志華、苗君易、鍾光民、周榮華、劉正芳, 2002, ``穿音速彈體側向噴流之空氣動力試驗研究,’’ 中華民國2002燃燒學會/民航學會/航太學會學術聯合會議論文集.

  23. Chung, K., 2001, ``Surface Roughness on Transonic Shock Wave/Turbulent Boundary Layer Interactions,’’ 23rd International Symposium on Shock Waves, July 22-27, Fort Worth, Texas, USA.

  24. 鍾光民, 2001, ``穿音速凹槽與凸角流交互作用之研究,’’ 第三屆海峽二岸航空太空科技學術研討會論文集, 5月29-30日, 淡江大學, 171-177頁.

  25. Zinoviev, V., Chung, K, and Miau, J., 2001, ``Application of the Hilbert Transform for Compressible Turbulent Flows,’’ Proc. the 4th Pacific International Conference on Aerospace Science and Technology, May 21-23 Kaohsiung Taiwan, pp. 293-300.

  26. Chung, K., 2001, ``A Study of Transonic Convex-Corner Flows,’’ Proc. the 2nd Indonesian-Taiwan Workshop on Science, Technology and Industry of Aeronautics, Kaohsiung Taiwan, May 21, pp. 73-80.

  27. Chung, K., 2001, ``An Experimental Study of Expansion-Corner Flows,’’ Proc. Experimental and Computational Workshop on Shock Wave Research, March 19-21, pp. 231-248, National Cheng Kung University.

  28. 周宏聲, 李佳峰, 苗君易, 鍾光民, 黃守仁, 劉瑞祥, 鍾武錕, 2001, ``在成大發展壓力感測塗料量測技術之初步報告,’’ 中華民國2001燃燒學會/民航學會/航太學會學術聯合會議論文集, 3月17日, AA67-AA74頁

  29. Chung, K., 2001, ``An Experimental Study of Compressible Rectangular Cavity Flows,’’ Proc. 2001 CIROC/CSAS/AASRC Joint Conference, March 17, pp. AA41-AA48.

  30. Zinoviev, V.N., Lebiga, V.A., Chung, K. and Miau, J., 2001, `` Application of Hot-Wire Technique in a Blowdown Type Transonic Wind Tunnel,’’ 39th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2001-0308.

  31. 邱文斌, 苗君易, 鍾光民, 周榮華, 2000, ``高攻角彈體空氣動力特性之研究,’’ 笫24屆全國應用力學研討會, 中原大學.

  32. Chung, K., 2000, ``An Experimental Study of Expansion-Corner Flows,’’ Proc. the 1st Indonesian-Taiwan Workshop on Science, Technology and Industry of Aeronautics, Jakarta Indonesia, July 18-19, pp. 114-119.

  33. Chung, K., 2000, ``Investigation on Unseparated and Separated Transonic Convex-Corner Flows,’’ 38th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2000-0917.

  34. 周大偉, 苗君易, 鍾光民, 周榮華，1999，穿音速風洞二維洞壁干擾研究，1999中華民國「航太學會/燃燒學會/民航學會」航太學術聯合會議論文集，中正理工學院，12月4日, 17-24頁

  35. Chung, K., 1999, ``A Study of Transonic Rectangular Cavity Flow of Varying Dimensions,’’ 5th AIAA/CEAS Aeroacoustics Conference, AIAA Paper 99-1909.

  36. Chung, K., 1998, ``Shock Wave and Turbulent Boundary Layer Interactions at Expansion Corner,’’ Proc. the 22nd National Conference in Theoretical and Applied Mechanics, Vol. 1, pp. 213-220.

  37. 陳昭銘, 苗君易, 鍾光民, 周榮華, 1998, ``表面粗糙物對穿音速邊界層之影響’’ 第四十屆中國航空太空學會學術研討會論文集, 33-40頁.

  38. Miau, J., Cheng, J., Chou, T., Chung, K., and Chou, J., 1998, ``The Effect of Surface Roughness on the Boundary Layer Transition,’’ Proc. the 7th International Symposium in Flow Modeling and Turbulent Measurement, ISFMTM98’, pp. 609-616.

  39. Chung, K., 1998, ``Measurements of Fluctuating Pressure of Transonic Cavity Flows,’’ ASME Fluids Engineering Division, Summer Meeting, June 21-25, FEDSM Paper 98-4943.

  40. 張國治, 鍾光民, 苗君易, 周榮華, 1998, ``穿音速機翼之表面視流觀察,’’ 第八屆中國燃燒科技學術研討會論文集, 527-530頁.

  41. Chung, K., 1997, ``Investigation on a Low-Supersonic Expansion Corner Flow,’’ Proc. the 39th Conference Aeronautical and Astronautical Society, ROC, pp. 385-390.

  42. Chung, K., 1997, ``Pressure Fluctuations of Transonic Turbulent Boundary Layer past Convex Corners,’’ Proc. the 3rd Pacific International Conference on Aerospace Science and Technology, pp. 38-42.

  43.  Chung, K., Chang, K., Miau, J. and Chou, J., 1997, ``A Study of a Transonic Wing for Laminar and Turbulent Flows,’’ Proc. the 3rd Pacific International Conference on Aerospace Science and Technology, pp. 176-181.

  44. 張國治, 鍾光民, 苗君易, 周榮華, 1996, ``穿音速機翼之表面視流觀察研究,’’ 第三十八屆中國航空太空學會學術研討會論文集, 19-28頁.

  45. 張國治, 鍾光民, 苗君易, 周榮華, 1995, ``穿音速機翼與翼梢小翼之尾流研究,’’ 第一屆海峽航空太空學術研討會論文集, 169-177頁.

  46. Chung, K. and Miau, J., 1995, ``Calibration of ASTRC/NCKU 600 mm x 600 mm Transonic Wind Tunnel,’’ 33rd AIAA Aerospace Science Meeting and Exhibit, Reno, USA , AIAA Paper 95-0238.

  47. Chung, K., Miau, J., 1994, ``Development and Operation of ASTRC/NCKU 600 mm Square Transonic Wind Tunnel,’’ Proc. 1994 International Conference on the Methods of Aerophysics Research, Part 1, pp. 72-77, Russia.

  48. Chung, K., Miau, J. and Yeh, J., 1994, ``Initial Operation of ASTRC/NCKU Transonic Wind Tunnel,’’ AIAA Paper 94-2515.

  49. 葉俊賢, 苗君易, 鍾光民, 周榮華, 1994, ``國立成功大學航太中心穿音速風洞校驗,’’ 第三十六屆中國航空太空學會學術研討會論文集, 259-268頁.

  50. Miau, J., Wen, R. and Chung, K., 1993, ``Transonic Flight Simulation in the IAA/NCKU 600 mm Square Transonic Wind Tunnel,’’ Proc. the 1st Pacific International Conference on Aerospace Science and Technology, Vol. 2, pp. 996-997

  51. Chung, K. and Lu, F.K., 1993, ``Incident Shock Wave/Turbulent Boundary Layer Interaction in a Hypersonic Flow,’’ Proc. the 1st Pacific International Conference on Aerospace Science and Technology, Vol. 2, pp. 653-660.