[1] Qiu X G, Han F H. Anti-icing system of aircraft[M]. Beijing: Aviation Professional Teaching Materials Editing Group, 1985: 23. (in Chinese) 裘燮纲, 韩凤华. 飞机防冰系统[M]. 北京: 航空专业教材编审组, 1985: 23.[2] Kind R J, Potapczuk M G, Feo A, et al. Experimental and computational simulation of in-flight icing phenomena[J]. Progress in Aerospace Sciences, 1998, 34(5-6): 257-345.[3] Aero-Engine Design Manual Editorial Board. Aero engine design manual, Volume 16[M]. Beijing: Aviation Industry Press, 2001: 251-254. (in Chinese) 《航空发动机设计手册》总编委会. 航空发动机设计手册——第16册[M]. 北京: 航空工业出版社, 2001: 251-254.[4] Al-Khalil K M, Keith T G, de Witt K J, et al. Thermal analysis of engine inlet anti-icing systems[J]. Journal of Propulsion and Power, 1990, 6(5): 628-634.[5] Potapczuk M G. A review of NASA Lewis' development plans for computational simulation of aircraft icing, AIAA-1999-0243. Reston: AIAA, 1999.[6] Saeed F, Morency F, Paraschivoiu I. Numerical simulation of a hot-air anti-icing system, AIAA-2000-0630. Reston: AIAA, 2000.[7] Hamed A, Das K, Basu D. Numerical simulations of ice droplet trajectories and collection efficiency on aero-engine rotating machinery, AIAA-2005-1248. Reston: AIAA, 2005.[8] Jorgenson P C E, Veres J P, May R D, et al. Aerospace engine icing modeling and simulation (Part I): ice crystal accretion on compression system components and modeling its effects on engine performance//SAE 2011 International Conference on Aircraft and Engine Icing and Ground Deicing, 2011: 1-26.[9] Yeoman K E. Efficiency of a bleed air powered inlet icing protective system, AIAA-1994-0717. Reston: AIAA, 1994.[10] Jin W, Taghavi R. A computational study of icing effects on the performance of S-duct inlets, AIAA-2008-4584. Reston: AIAA, 2008.[11] Lee S, Loth E, Simulation of icing on a cascade of stator blades, AIAA-2006-0208. Reston: AIAA, 2006.[12] Ashwood P F. An altitude test facility for large turbofan engines, AIAA-1972-1069. Reston: AIAA, 1972.[13] Luttrell J, West T. F-22 inlet shed ice particle sizing test, AIAA-2001-0553. Reston: AIAA, 2001.[14] Willcocks H J. Icing conditions on sea level gas turbine engine test stands, AIAA-1982-1237-631. Reston: AIAA, 1982.[15] Al-Khalil K M, Hitzigrath R, Philippi O, et al. Icing analysis and test of a business jet engine inlet duct, AIAA-2000-1040-453. Reston: AIAA, 2000.[16] Venkataramani K S, Balan C, Caney R D, et al. Wind tunnel tests and modeling studies of ice accretion relevant to aircraft engines, AIAA-2003-0906. Reston: AIAA, 2003.[17] Zhang D L, Chen W J. Numerical simulation of rime ice accretion process on airfoil[J]. Journal of Aerospace Power, 2004,19(1): 137-141. (in Chinese) 张大林, 陈维健. 飞机机翼表面霜状冰结冰过程的数值模拟[J]. 航空动力学报, 2004, 19(1): 137-141.[18] Yi X. Numerical computation of aircraft icing and study on icing test scaling law. Mianyang: China Aerodynamics Research and Development Center, 2007. (in Chinese) 易贤. 飞机积冰的数值计算与积冰试验相似准则研究. 绵阳: 中国空气动力研究与发展中心, 2007.[19] Bu X Q, Lin G P, Yu J. Three-dimensional conjugate heat transfer simulation for the surface temperature of wing hot-air anti-icing system[J]. Journal of Aerospace Power, 2009, 24(11): 2495-2500. (in Chinese) 卜雪琴, 林贵平, 郁嘉. 三维内外热耦合计算热气防冰系统表面温度[J]. 航空动力学报, 2009, 24(11): 2495-2500.[20] Chang S N, Su X M, Qiu Y F. Ice accretion simulation on three dimensional wings[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(2): 212-222. (in Chinese) 常士楠, 苏心明, 邱义芬. 三维机翼结冰模拟[J]. 航空学报, 2011, 32(2): 212-222.[21] Dong W, Zhu J J, Zhao Q Y. Numerical simulation of the guide vane with hot air anti-icing passage, AIAA-2011-3944. Reston: AIAA, 2011.[22] Dong W, Hou Y Z, Min X H. Experimental study of hot air anti-icing system of inlet guide vane[J]. Journal of Shanghai Jiao Tong University, 2010, 44(11): 1579-1582. (in Chinese) 董威, 侯玉柱, 闵现花. 进口导向叶片热气防冰系统试验研究[J]. 上海交通大学学报, 2010, 44(11): 1579-1582. |