空军工程大学学报(自然科学版) 11年 [8 Wright William B, Bidwell Colin S. Additional improvements to the NASA lewis ice accretion code LEWICE[R]. AIAA 95 0752 [9 Chirag Bhargava, Eric Loth, Mar zuk. Aerodynamic simulations of the NASA Glenn icing research tunnel[r]. AIAa [10 Patrick Hancir, Eric Loth. Computations of droplet distributions in an icing research tunnel[ r]. AlAA 99-0097 [11 Bidwell C S, Mohler. Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wind, a swept NASA0012 wing tip, an axisymmetric inlet and a boeing 737-200 inlet[R]. NASA TM-106821, 1995 [12 Al-Khalil K M, Keith T G, De Witt K J. Icing calculations on a typical commercial jet engine inlet nacelle[ J]. Joumal of aircraft,1997,34(1):87-92 [13 Snellen M, Boelens O J, Hoeijmakers. A computational method for numerically simulating ice accretion[R]. AIAA 9 2206. [14 Suikno Wirogo, Shashidhar Sriramblatla. An Eulerian method to calculate the collection efficiency on two and three dimensional bodies[ R]. AlAA 2003-1073 [15 Anderson David N, Jen Ching Tsao Evaluation and validation of the messenger freezing fraction [R. AIAA 2003-1218. [16]常土楠,艾素霄.一种飞机机翼表面结冰过程仿真方法[J].系统仿真学报,2008,20(10):2538-2545. CHANG Shinan, AI Suxiao. Simulation approach of ice accretion on airfoil surface[J]. Journal of system simulation, 2008,20 (10):2538-2545 [17 Kaushik Das. Numerical simulations of icing in turbo machinery[D]. Cincinnati Division of research and advanced studies of e university of Cincinnati, 2006 (编辑:徐敏) Research Evolvement on Icing of Aircraft Engine XING Yu-ming, LIU Hai-li, XU Liu -qing School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijin 100191, China) Abstract: The test capability of AEDC and CIRA icing wind tunnel are analyzed. The present situation of buildi the icing wind tunnel and that of icing test in China are analyzed. The measurements of the important parameters of liquid water content(LWC)and the water droplets median volume diameter(MVD)are researched. In numerical imulation aspect, four parts of icing numerical calculation are summarized, the virtues and defects of different methods are compared. At last, the development trend of the research for icing on aircraft engine is put forward based on the current research actualities Key words: engine; icing wind -tunnel; measure technique; numerical calculation［８］ Ｗｒｉｇｈｔ Ｗｉｌｌｉａｍ Ｂ， Ｂｉｄｗｅｌｌ Ｃｏｌｉｎ Ｓ．Ａｄｄｉｔｉｏｎａｌ ｉｍｐｒｏｖｅｍｅｎｔｓ ｔｏ ｔｈｅ ＮＡＳＡ ｌｅｗｉｓ ｉｃｅ ａｃｃｒｅｔｉｏｎ ｃｏｄｅ ＬＥＷＩＣＥ［Ｒ］．ＡＩＡＡ ９５ － ０７５２． ［９］ Ｃｈｉｒａｇ Ｂｈａｒｇａｖａ， Ｅｒｉｃ Ｌｏｔｈ， Ｍａｒｋ Ｐｏｔａｐｃｚｕｋ．Ａｅｒｏｄｙｎａｍｉｃ ｓｉｍｕｌａｔｉｏｎｓ ｏｆ ｔｈｅ ＮＡＳＡ Ｇｌｅｎｎ ｉｃｉｎｇ ｒｅｓｅａｒｃｈ ｔｕｎｎｅｌ［Ｒ］．ＡＩＡＡ ２００３ －５６６． ［１０］ Ｐａｔｒｉｃｋ Ｈａｎｃｉｒ， Ｅｒｉｃ Ｌｏｔｈ．Ｃｏｍｐｕｔａｔｉｏｎｓ ｏｆ ｄｒｏｐｌｅｔ ｄｉｓｔｒｉｂｕｔｉｏｎｓ ｉｎ ａｎ ｉｃｉｎｇ ｒｅｓｅａｒｃｈ ｔｕｎｎｅｌ［Ｒ］．ＡＩＡＡ ９９ －００９７． ［１１］ Ｂｉｄｗｅｌｌ Ｃ Ｓ，Ｍｏｈｌｅｒ．Ｃｏｌｌｅｃｔｉｏｎ ｅｆｆｉｃｉｅｎｃｙ ａｎｄ ｉｃｅ ａｃｃｒｅｔｉｏｎ ｃａｌｃｕｌａｔｉｏｎｓ ｆｏｒ ａ ｓｐｈｅｒｅ，ａ ｓｗｅｐｔ ＭＳ（１） －３１７ ｗｉｎｄ，ａ ｓｗｅｐｔ ＮＡＳＡ００１２ ｗｉｎｇ ｔｉｐ，ａｎ ａｘｉｓｙｍｍｅｔｒｉｃ ｉｎｌｅｔ ａｎｄ ａ ｂｏｅｉｎｇ ７３７ －２００ ｉｎｌｅｔ［Ｒ］．ＮＡＳＡ ＴＭ －１０６８２１，１９９５． ［１２］ Ａｌ －Ｋｈａｌｉｌ Ｋ Ｍ， Ｋｅｉｔｈ Ｔ Ｇ， Ｄｅ Ｗｉｔｔ Ｋ Ｊ．Ｉｃｉｎｇ ｃａｌｃｕｌａｔｉｏｎｓ ｏｎ ａ ｔｙｐｉｃａｌ ｃｏｍｍｅｒｃｉａｌ ｊｅｔ ｅｎｇｉｎｅ ｉｎｌｅｔ ｎａｃｅｌｌｅ［ Ｊ］．Ｊｏｕｒｎａｌ ｏｆ ａｉｒｃｒａｆｔ， １９９７， ３４（１）：８７ －９２． ［１３］ Ｓｎｅｌｌｅｎ Ｍ， Ｂｏｅｌｅｎｓ Ｏ Ｊ， Ｈｏｅｉｊｍａｋｅｒｓ．Ａ ｃｏｍｐｕｔａｔｉｏｎａｌ ｍｅｔｈｏｄ ｆｏｒ ｎｕｍｅｒｉｃａｌｌｙ ｓｉｍｕｌａｔｉｎｇ ｉｃｅ ａｃｃｒｅｔｉｏｎ［Ｒ］．ＡＩＡＡ ９７ － ２２０６． ［１４］ Ｓｕｉｋｎｏ Ｗｉｒｏｇｏ， Ｓｈａｓｈｉｄｈａｒ Ｓｒｉｒａｍｂｌａｔｌａ．Ａｎ Ｅｕｌｅｒｉａｎ ｍｅｔｈｏｄ ｔｏ ｃａｌｃｕｌａｔｅ ｔｈｅ ｃｏｌｌｅｃｔｉｏｎ ｅｆｆｉｃｉｅｎｃｙ ｏｎ ｔｗｏ ａｎｄ ｔｈｒｅｅ ｄｉｍｅｎｓｉｏｎａｌ ｂｏｄｉｅｓ［Ｒ］．ＡＩＡＡ ２００３ －１０７３． ［１５］ Ａｎｄｅｒｓｏｎ Ｄａｖｉｄ Ｎ，Ｊｅｎ Ｃｈｉｎｇ Ｔｓａｏ．Ｅｖａｌｕａｔｉｏｎ ａｎｄ ｖａｌｉｄａｔｉｏｎ ｏｆ ｔｈｅ ｍｅｓｓｅｎｇｅｒ ｆｒｅｅｚｉｎｇ ｆｒａｃｔｉｏｎ ［Ｒ］．ＡＩＡＡ ２００３ －１２１８． ［１６］ 常士楠，艾素霄．一种飞机机翼表面结冰过程仿真方法［Ｊ］．系统仿真学报，２００８，２０（１０）：２５３８ －２５４５． ＣＨＡＮＧ Ｓｈｉｎａｎ， ＡＩ Ｓｕｘｉａｏ．Ｓｉｍｕｌａｔｉｏｎ ａｐｐｒｏａｃｈ ｏｆ ｉｃｅ ａｃｃｒｅｔｉｏｎ ｏｎ ａｉｒｆｏｉｌ ｓｕｒｆａｃｅ［Ｊ］．Ｊｏｕｒｎａｌ ｏｆ ｓｙｓｔｅｍ ｓｉｍｕｌａｔｉｏｎ， ２００８，２０ （１０）：２５３８ －２５４５． ［１７］ Ｋａｕｓｈｉｋ Ｄａｓ．Ｎｕｍｅｒｉｃａｌ ｓｉｍｕｌａｔｉｏｎｓ ｏｆ ｉｃｉｎｇ ｉｎ ｔｕｒｂｏ ｍａｃｈｉｎｅｒｙ［Ｄ］．Ｃｉｎｃｉｎｎａｔｉ：Ｄｉｖｉｓｉｏｎ ｏｆ ｒｅｓｅａｒｃｈ ａｎｄ ａｄｖａｎｃｅｄ ｓｔｕｄｉｅｓ ｏｆ ｔｈｅ ｕｎｉｖｅｒｓｉｔｙ ｏｆ Ｃｉｎｃｉｎｎａｔｉ，２００６． （编辑：徐敏） Research Evolvement on Icing of Aircraft Engine ＸＩＮＧ Ｙｕ －ｍｉｎｇ， ＬＩＵ Ｈａｉ －ｌｉ， ＸＵ Ｌｉｕ －ｑｉｎｇ （Ｓｃｈｏｏｌ ｏｆ Ａｅｒｏｎａｕｔｉｃ Ｓｃｉｅｎｃｅ ａｎｄ Ｅｎｇｉｎｅｅｒｉｎｇ， Ｂｅｉｊｉｎｇ Ｕｎｉｖｅｒｓｉｔｙ ｏｆ Ａｅｒｏｎａｕｔｉｃｓ ａｎｄ Ａｓｔｒｏｎａｕｔｉｃｓ， Ｂｅｉｊｉｎｇ １００１９１， Ｃｈｉｎａ） Abstract：Ｔｈｅ ｔｅｓｔ ｃａｐａｂｉｌｉｔｙ ｏｆ ＡＥＤＣ ａｎｄ ＣＩＲＡ ｉｃｉｎｇ ｗｉｎｄ ｔｕｎｎｅｌ ａｒｅ ａｎａｌｙｚｅｄ．Ｔｈｅ ｐｒｅｓｅｎｔ ｓｉｔｕａｔｉｏｎ ｏｆ ｂｕｉｌｄｉｎｇ ｔｈｅ ｉｃｉｎｇ ｗｉｎｄ ｔｕｎｎｅｌ ａｎｄ ｔｈａｔ ｏｆ ｉｃｉｎｇ ｔｅｓｔ ｉｎ Ｃｈｉｎａ ａｒｅ ａｎａｌｙｚｅｄ．Ｔｈｅ ｍｅａｓｕｒｅｍｅｎｔｓ ｏｆ ｔｈｅ ｉｍｐｏｒｔａｎｔ ｐａｒａｍｅｔｅｒｓ ｏｆ ｌｉｑｕｉｄ ｗａｔｅｒ ｃｏｎｔｅｎｔ （ＬＷＣ） ａｎｄ ｔｈｅ ｗａｔｅｒ ｄｒｏｐｌｅｔｓ ｍｅｄｉａｎ ｖｏｌｕｍｅ ｄｉａｍｅｔｅｒ （ＭＶＤ） ａｒｅ ｒｅｓｅａｒｃｈｅｄ．Ｉｎ ｎｕｍｅｒｉｃａｌ ｓｉｍｕｌａｔｉｏｎ ａｓｐｅｃｔ， ｆｏｕｒ ｐａｒｔｓ ｏｆ ｉｃｉｎｇ ｎｕｍｅｒｉｃａｌ ｃａｌｃｕｌａｔｉｏｎ ａｒｅ ｓｕｍｍａｒｉｚｅｄ， ｔｈｅ ｖｉｒｔｕｅｓ ａｎｄ ｄｅｆｅｃｔｓ ｏｆ ｄｉｆｆｅｒｅｎｔ ｍｅｔｈｏｄｓ ａｒｅ ｃｏｍｐａｒｅｄ．Ａｔ ｌａｓｔ， ｔｈｅ ｄｅｖｅｌｏｐｍｅｎｔ ｔｒｅｎｄ ｏｆ ｔｈｅ ｒｅｓｅａｒｃｈ ｆｏｒ ｉｃｉｎｇ ｏｎ ａｉｒｃｒａｆｔ ｅｎｇｉｎｅ ｉｓ ｐｕｔ ｆｏｒｗａｒｄ ｂａｓｅｄ ｏｎ ｔｈｅ ｃｕｒｒｅｎｔ ｒｅｓｅａｒｃｈ ａｃｔｕａｌｉｔｉｅｓ． Key words：ｅｎｇｉｎｅ； ｉｃｉｎｇ ｗｉｎｄ －ｔｕｎｎｅｌ； ｍｅａｓｕｒｅ ｔｅｃｈｎｉｑｕｅ； ｎｕｍｅｒｉｃａｌ ｃａｌｃｕｌａｔｉｏｎ １２ 空军工程大学学报（自然科学版） ２０１１ 年