[1] Qiu X G, Han F H. Aircraft anti-icing system. Beijing: Compilation and Examination Group of Aero Specialized Teaching Materials, 1985. (in Chinese) 裘燮纲, 韩凤华. 飞机防冰系统. 北京: 航空专业教材编审组, 1985.
[2] Al-Khalil K M, Keith T G, Jr, De Witt K J. Icing calculations on a typical commercial jet engine inlet nacelle. Journal of Aircraft, 1997, 34(1): 87-93.
[3] Bidwell C S, Mohler S R. Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet. AIAA-1995-755, 1995.
[4] Al-Khalil K, Hitzigratht R, Philippit O, et al. Icing analysis and test of a business jet engine inlet duct. AIAA-2000-1040, 2000.
[5] Schuster E P, Gambill J M, Fisher M S. Computational icing analysis of aircraft inlets. AIAA-1992-3178, 1992.
[6] Bidwell C S, Potapczuk M G. Users manual for the NASA lewis three-dimensional ice accretion code (LEWICE3D). NASA TM-105974, 1993.
[7] Beaugendre H, Morency F, Habashi W G. ICE3D, FENSAP-ICE'S 3D in-flight ice accretion module. AIAA-2002-0385, 2002.
[8] Papadakis M. Comparison of experimental and computational ice shapes for an engine inlet. AIAA-2010-7671, 2010.
[9] Newmerical Technologies Int. FENSAP-ICE 2011 manual. Canada: Newmerical Technologies Int., 2011.
[10] Yi X, Gui Y W, Zhu G L. Numerical method of a three-dimensional ice accretion model of aircraft. Acta Aeronautica et Astronautica Sinica, 2010, 31(11): 2152-2158. (in Chinese) 易贤, 桂业伟, 朱国林. 飞机三维结冰模型及其数值求解方法. 航空学报, 2010, 31(11): 2152-2158.
[11] Chang S N, Su X M, Qiu Y F. Ice accretion simulation on three dimensional wings. Acta Aeronautica et Astronautica Sinica, 2011, 32(2): 212-222. (in Chinese) 常士楠, 苏新明, 邱义芬.三维机翼结冰模拟. 航空学报, 2011, 32(2): 212-222.
[12] Hu Y P. Numerical simulation of ice accretion on aero-engine entry components. Nanjing: College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, 2008. (in Chinese) 胡娅萍. 航空发动机进口部件积冰的数值模拟研究. 南京: 南京航空航天大学能源与动力学院, 2008.
[13] Yang S H, Lin G P. Numerical simulation of ice accretion on airfoils. Journal of Aerospace Power, 2011, 26(2): 323-330. (in Chinese) 杨胜华, 林贵平. 机翼结冰过程的数值模拟. 航空动力学报, 2011, 26(2): 323-330.
[14] Yang S H. Two-dimensional in-flight ice accretion simulation. Beijing: School of Aeronautic Science and Engineering, Beihang University, 2010. (in Chinese) 杨胜华. 二维飞机结冰过程仿真. 北京: 北京航空航天大学航空科学与工程学院, 2010.
[15] ANSYS Inc. ANSYS fluent 12.0 UDF manual. New Hapmpshire: ANSYS Inc., 2009.
[16] Shen X B, Lin G P, Yang S H. Analysis on three dimensional water droplets impingement characteristics of engine inlet. Journal of Beijing University of Aeronautics and Astronautics, 2011, 31(1): 1-5.(in Chinese) 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. 北京航空航天大学学报, 2011, 31(1): 1-5. |