Application of CFD Method on Engine Nacelle Anti-icing System
HUA Rui-rui;LI Zhi-mao;TAN Zheng-wen;XU Jia-jia;Environment Control and Oxygen System Department, Shanghai Aircraft Design and Research Institute;
According to airworthiness standards, civil airplane must be able to safely operate in the continuous maximum and intermittent maximum icing conditions of appendix C. An analysis must be performed to establish that the ice protection for the various components of the airplane is adequate. To evaluate the performance of specific engine nacelle anti-icing system in icing conditions of appendix C, this paper utilize A CFD method developed by Shanghai Aircraft Design and Research Institute.
【CateGory Index】： V244.15