3D Numerical Simulation of Ice Accretion on a Rotating Surface

被引:5
作者
Mu, Zuodong [1 ]
Lin, Guiping [1 ]
Bai, Lizhan [1 ]
Shen, Xiaobin [1 ]
Bu, Xueqin [1 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Lab Fundamental Sci Ergon & Environm Control, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
Aircraft icing; Water film runback; Numerical simulation; Rotating; ENGINE INLET; MODEL;
D O I
10.5139/IJASS.2017.18.2.352
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A novel 3D mathematical model for water film runback and icing on a rotating surface is established in this work, where both inertial forces caused by the rotation and shear forces due to the air flow are taken into account. The mathematical model of the water film runback and energy conservation of phase transition process is established, with a cyclical average method applied to simulate the unsteady parameters variation at angles of attack. Ice accretion on a conical spinner surface is simulated and the results are compared with the experimental data to validate the presented model. Then Ice accretion on a cowling surface is numerically investigated. Results show that a higher temperature would correspond to a larger runback ice area and thinner ice layer for glaze ice. Rotation would enhance the icing process, while it would not significantly affect the droplet collection efficiency for an axi-symmetric surface. In the case at angle of attack, the effect of rotation on ice shape is appreciable, ice would present a symmetric shape, while in a stationary case the shape is asymmetric.
引用
收藏
页码:352 / 364
页数:13
相关论文
共 27 条
[1]  
Al-Khalil K., 1997, P 35 AER SCI M EXH R, DOI [10.2514/6.1997-51, DOI 10.2514/6.1997-51]
[2]   Icing calculations on a typical commercial jet engine inlet nacelle [J].
AlKhalil, KM ;
Keith, TG ;
DeWitt, KJ .
JOURNAL OF AIRCRAFT, 1997, 34 (01) :87-93
[3]  
Anderson JD, 2016, Fundamentals of Aerodynamics, V6th
[4]  
Baruzzi G., 2003, AIAA20030024, DOI [10.2514/6.2003-24, DOI 10.2514/6.2003-24]
[5]   Development of a second generation in-flight icing simulation code [J].
Beaugendre, H ;
Morency, F ;
Habashi, WG .
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2006, 128 (02) :378-387
[6]   FENSAP-ICE's three-dimensional in-flight ice accretion module: ICE3D [J].
Beaugendre, H ;
Morency, F ;
Habashi, WG .
JOURNAL OF AIRCRAFT, 2003, 40 (02) :239-247
[7]  
Belz R.A., 1986, AIAA PAPER, P1647, DOI [10.2514/6.1986-1647, DOI 10.2514/6.1986-1647]
[8]   Experimental study of icing accretion on a rotating conical spinner [J].
Chen, Ningli ;
Ji, Honghu ;
Hu, Yaping ;
Wang, Jian ;
Cao, Guangzhou .
HEAT AND MASS TRANSFER, 2015, 51 (12) :1717-1729
[9]  
Cristhian N. A., 2011, J AIRCRAFT, V48, P119, DOI [10.2514/1.0000327, DOI 10.2514/1.0000327]
[10]  
David S., 2014, 32 ASME WIND EN S NA, DOI [10.2514/6.2014-1399, DOI 10.2514/6.2014-1399]