Design and calculation for the anti-icing system of an aircraft engine let

[1] 裘燮纲,韩凤华.飞机防冰系统[M].北京:航空专业教材审编组,1985 Qiu Xiangang, Han Fenghua. Aircraft anti-icing system[M]. Beijing:Compilation and Examination Group of Aero Specialized Teching Materials, 1985(in Chinese) [2] 常士楠,韩凤华.飞机发动机进气道前缘热气防冰器性能分析[J].北京航空航天大学学报, 1999, 25(2):201-203 Chang Shinan, Han Fenghua. Performance anslysis on hot-air anti-icer of airplane engine inlet[J]. Journal of Beijing University of Aeronautics and Astronautics,1999,25(2):201-203(in Chinese) [3] 杨倩,常士楠,袁修干. 发动机进气道水滴撞击特性分析[J].北京航空航天大学学报, 2002,28(3):362-365 Yang Qian, Chang Shinan,Yuan Xiugan. Analysis on droplet trajectories of an engine inlet[J].Journal of Beijing University of Aeronautics and Astronautics,2002,28(3):362-365(in Chinese) [4] Morency F, Tezok F, Paraschivoiu I. Heat and mass transfer in the case of an anti-icing system modelisation . AIAA-99-0623,1999 [5] Thomas S K, Cassoni R P. Aircraft anti-icing and de-icing techniques and modeling[J]. Journal of Aircraft, 1996,33(5):841-854