裘燮纲,韩凤华.飞机防冰系统[M].北京:航空专业教材编审组,1985:50-53Qiu Xiegang,Han Fenghua.Aircraft anti-icing system[M].Beijing:Compilation and Examination Group of Aero Specialized Teaching Materials,1985:50-53(in Chinese)
[2]
周力行.湍流气粒两相流动和燃烧的理论与数值模拟[M].北京:科学出版社,1994:293-298Zhou Lixing.Theory and numerical modeling of turbulent gas-particle flows and combustion[M].Beijing:Science Press,1994:293-298(in Chinese)
[3]
杨倩,常士楠,袁修干.水滴撞击特性的数值计算方法研究[J].航空学报,2002,23(2):173-176 Yang Qian,Chang Shinan,Yuan Xiugan.Study on numerical method for determining the droplet trajectories[J].Acta Aeronuatica et Astronautica Sinca,2002,23(2):173-176(in Chinese)
[4]
常士楠,苏新明,邱义芬.三维机翼结冰模拟[J].航空学报,2011,32(2):212-222 Chang Shinan,Su Xinming,Qiu Yifen.Ice accretion simulation on three dimensional wings[J].Acta Aeronautica et Astronautica Sinca,2011,32(2):212-222(in Chinese)
[5]
申晓斌,林贵平,杨胜华.三维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,2011,37(1):1-5 Shen Xiaobin,Lin Guiping,Yang Shenghua.Analysis on three dimensional water droplets impingement characteristics of engine inlet[J].Journal of Beijing University of Aeronautics and Astronautics,2011,37(1):1-5(in Chinese)
[6]
Bourgault Y,Boutanios Z,Habashi W G.Three-dimensional eulerian approach to droplet impingement simulation using FENSAP-ICE,part 1:model, algorithm, and validation[J].Journal of Aircraft,2000,37(1):95-103
[7]
赵秋月,董威,朱剑鋆.发动机旋转整流帽罩的水滴撞击特性分析[J].燃气涡轮试验与研究,2011,24(4):32-35 Zhao Qiuyue,Dong Wei,Zhu Jianjun.Droplets impinging characteristic analysis of the rotating fairing of aero-engine[J].Gas Turbine Experiment and Research,2011,24(4):32-35(in Chinese)
[8]
Das K,Hamed A,Basu D.Ice shape prediction for turbofan rotating blades[R].AIAA 2006-0209,2006
[9]
杨胜华,林贵平,申晓斌.三维复杂表面水滴撞击特性计算[J].航空动力学报,2010,25(2):284-290 Yang Shenghua,Lin Guiping,Shen Xiaobin.Water droplet impingement prediction for three-dimensional complex surfaces[J].Journal of Aerospace Power,2010,25(2):284-290(in Chinese)
[10]
Slater S A,Young J B.The calculation of inertial particle transport in dilute gas-particle flows[J].International Journal of Multiphase Flow,2001,27(1):61-87
[11]
Wirogo S,Srirambhatla S.An Eulerian method to calculate the collection efficiency on two and three dimensional bodies[R].AIAA 2003-1073,2003
[12]
Tong X,Luke E A.Eulerian simulation of icing collection efficiency using a singularity diffusion model[R].AIAA 2005-1246,2005
[13]
Cao Y,Ma C,Zhang Q,et al.Numerical simulation of ice accretions on an aircraft wing[J].Aerospace Science and Technology,2012,23(1):296-304
[14]
Linke D A.Systems of commercial turbofan engines[M].Berlin:Springer,2008:179-183
[15]
李西园.旋转部件结冰缩比试验相似性研究[D].北京:北京航空航天大学,2010 Li Xiyuan.Similarity of icing scaling test for aircraft rotating components[D].Beijing:Beijing University of Aeronautics and Astronautics,2010(in Chinese)