| [1] Gelder T F. Droplet impingement and ingestion by supersonic nose inlet in subsonic tunnel conditions. NACA TN 4268, 1958.[2] Papadakis M, Elangonan R, Freund G A, et al. An experimental method for measuring water droplet impingement efficiency on two- and three-dimensional bodies. NASA CR 4257, 1989.[3] Papadakis M, Rachman A, Wong S C. Water impingement experiments on a NACA 23012 airfoil with simulated glaze ice shapes. AIAA-2004-565, 2004.[4] Liu D Y, Han Y H, Ding L, et al. Dynamic image processing measurement method of droplets impingement characteristics. Journal of Aerospace Power, 2012, 27(5): 986-992.(in Chinese) 刘丹阳, 韩雅慧, 丁立, 等.水滴撞击特性参数的动态图像处理测量方法.航空动力学报, 2012, 27(5): 986-992.[5] Beaugendre H, Morency F, Habashi W G. Development of a second generation in-flight icing simulation code. Journal of Fluids Engineering, 2006, 128(2): 378-387.[6] Wright W B. Users manual for the improved NASA Lewi-s ice accretion code LEWICE 1.6.NASA CR 198355, 1995.[7] Gent R W. TRAJICE2-A combined water droplet and ice accretion prediction code for airfoils. Royal Aerospace Establishment, TR90054, 1990.[8] Hedde T, Guffond D. Improvement of the ONERA 3-D icing code, comparison with 3D experimental shapes. AIAA-1993-169, 1993.[9] Silveira R A, Maliska C R, Estivam, D A, et al. Evaluation of collection efficiency methods for icing analisys. COBEM2003-1810, 2003.[10] Yang Q, Chang S N, Yuan X G. Study on numerical method for determining the droplet trajectries. Acta Aeronautica et Astronautica Sinica, 2002, 23 (2): 173-176. (in Chinese) 杨倩, 常士楠, 袁修干.水滴撞击特性的数值计算方法研究.航空学报, 2002, 23(2): 173-176.[11] Ke P, Zhang S G, Wu J H, et al. An improved known vicinity algorithm based on geometry test for particle localization in arbitrary grid. Journal of Computional Physics, 2009, 228(46): 9001-9019.[12] Zhang Q, Hu L, Cao Y H. Three-dimensional numerical simulation of supercooled droplets impinging on a wing. Journal of Aerospace Power, 2009, 24(6): 1345-1350. (in Chinese) 张强, 胡利, 曹义华. 过冷水滴撞击三维机翼的数值模拟.航空动力学报, 2009, 24(6): 1345-1350.[13] Yang S H, Lin G P, Shen X B. Water droplet impingement prediction for three-dimensional complex surface. Journal of Aerospace Power, 2010, 25(2):284-290. (in Chinese) 杨胜华, 林贵平, 申晓斌. 三维复杂表面水滴撞击特性计算.航空动力学报, 2010, 25(2): 284-290.[14] Bu X Q, Lin G P. Predictions of collection efficiency and anti-icing surface temperature. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10): 1182-1185. (in Chinese) 卜雪琴, 林贵平. 基于CFD的水收集系数及防冰表面温度预测.北京航空航天大学学报, 2007, 33(10): 1182-1185.[15] Papadakis M, Elangonan R, Freund G A, Jr, et al.An experimental method for measuring water droplet im-pingement efficiency on two- and three-dimensional bodies. NASA CR 4257, 1989. |
CJA
