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基于润滑理论的二维积冰数值模拟

DOI: 10.13700/j.bh.1001-5965.2013.0625, PP. 1442-1450

Keywords: 润滑理论,薄膜流,积冰,翼型,传输线,数值模拟

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Abstract:

将基于润滑理论的水膜-冰层模型推广到在任意二维截面上建立的正交曲线坐标系,得到描述二维型线表面水膜流动和积冰的偏微分控制方程.采用一种隐式-显式有限差分格式建立控制方程组的代数形式,给出求解非稳态控制方程组的数值方法.为验证模型和数值解法的有效性,在典型的航空积冰和传输线积冰环境下对翼型和传输线表面的积冰算例进行数值模拟.将水膜-冰层模型的冰形计算结果与传统Messinger模型的模拟结果以及冰风洞试验结果进行对比,低温明冰条件下采用当前方法计算的翼型表面冰形接近于Messinger模型的模拟冰形曲线;相对高温条件下的计算结果比传统Messinger模型更为精确.低速积冰环境下Messinger模型难以模拟的传输线表面积冰同样可以采用水膜-冰层模型进行有效预测.

References

[1]  Messinger B L. Equilibrium temperature of an unheated icing surface as a function of air speed[J].Journal of the Aeronautical Sciences,1953,20(1):29-42
[2]  Ruff G A, Berkowitz B M.User's manual for the NASA lewis ice accretion prediction code (LEWICE)[R].NASA CR 1990-185129,1990
[3]  Myers T G, Hammond D W.A mathematical model for atmospheric ice accretion and water flow on a cold surface[J].International Journal of Heat and Mass Transfer,2004,47(25): 54835500
[4]  Myers T G, Charpin J P F,Chapman S J.The flow and solidification of a thin fluid film on an arbitrary three-dimensional surface[J].Physics of Fluids,2002,14(8):2788-2803
[5]  Gent R W, Dart N P,Cansdale J T.Aircraft icing[J].Philos Trans R Soc London,Ser A,2000,358:2873-2911
[6]  Verdin P, Charpin J P F,Thompson C P.Multistep results in ICECREMO2[J].Journal of Aircraft,2009,46(5):1607-1613
[7]  Verdin P, Charpin J P F.Multi-stepping ice prediction on cylinders and other relevant geometries[J].Journal of Aircraft,2013,50(3):871-878
[8]  Moriarty J A, Schwartz L W,Tuck E O. Unsteady spreading of thin liquid films with small surface tension[J].Physics of Fluids A,1991,3(5):733-742
[9]  Brakel T W, Charpin J P F.One-dimensional ice growth due to incoming supercooled droplets impacting on a thin conducting substrate[J].International Journal of Heat and Mass Transfer,2007,50(9/10):1694-1705
[10]  Wright W B, Gent R W,Guffond D.DRA/NASA/ONERA collaboration on icing research part IIprediction of airfoil ice accretion[R].NASA CR 1997-202349,1997
[11]  Spalart P R. Trends in turbulence treatments[J].AIAA Paper 2000-2306,2000
[12]  Shin J, Berkowitz B M.Prediction of ice shapes and their effect on airfoil performance[R].AIAA-91-0264,1991
[13]  Beaugendre H, Morency F,Habashi W G.Development of a second generation in-flight icing simulation code[J].Journal of Fluids Engineering,2006,128(2):378-387
[14]  张强,曹义华, 李栋.采用欧拉两相流法对翼型表面霜冰的数值模拟[J].北京航空航天大学学报,2009,35(3): 351355 Zhang Qiang,Cao Yihua,Li Dong.Numerical method to simulate rime ice accretions on an airfoil[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(3):351-355(in Chinese)
[15]  Wright W B. Validation results for LEWICE2.0[R].NASA/CR 1999-208690,1999
[16]  Fu P, Farzaneh M,Bouchard G.Two-dimensional modelling of the ice accretion process on transmission line wires and conductors[J].Cold Regions Science and Technology,2006,46(2):132-146
[17]  庄礼贤, 尹协远,马晖扬.流体力学[M].合肥:中国科学技术大学出版社,1991:401 Zhuang Lixian,Yin Xieyuan,Ma Huiyang.Fluid mechanics[M].Hefei:Unversity of Science and Technology of China Press,1991:401(in Chinese)

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