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多段翼构型的积冰数值模拟
引用本文:张强,高正红,傅林.多段翼构型的积冰数值模拟[J].航空动力学报,2011,26(7):1465-1470.
作者姓名:张强  高正红  傅林
作者单位:西北工业大学航空学院翼型、叶栅空气动力学国防科技重点实验室,西安,710072
摘    要:基于非结构网格提出一种针对多段翼构型的积冰数值模拟方法.通过求解气体欧拉方程得到多段翼的绕流流场,基于空气绕流流场的气流速度分布,采用迭代法对水滴控制方程进行数值求解,得到多段翼各翼面的水滴收集特性;采用不同的积冰冻结模型模拟霜冰和明冰的冻结过程;利用冰层时间推进法模拟积冰过程,基于积冰法向生长假设生成积冰外形.对某典...

关 键 词:积冰  过冷水滴  多段翼  非结构网格  两相流  数值模拟
收稿时间:2010/12/29 0:00:00
修稿时间:2011/3/21 0:00:00

Numerical simulation of ice accretions on multi-element airfoils
ZHANG Qiang,GAO Zheng-hong and FU Lin.Numerical simulation of ice accretions on multi-element airfoils[J].Journal of Aerospace Power,2011,26(7):1465-1470.
Authors:ZHANG Qiang  GAO Zheng-hong and FU Lin
Institution:ZHANG Qiang,GAO Zheng-hong,FU Lin(National Key Laboratory of Science and Technology on Aerodynamic Design and Research,School of Aeronautics,Northwestern Polytechnical University,Xi'an 710072,China)
Abstract:A numerical method based on unstructured grids was proposed to simulate ice accretions on multi-element airfoils.The air flowfield was solved using the Euler equations.Based on air velocity distribution,the governing equations for droplets were solved using an iterative method to obtain the collection efficiency.The different freezing models corresponding to the rime and glaze ice were employed to simulate the freezing process.The process of ice accretions was simulated with the assumption that ice accumula...
Keywords:ice accretions  supercooled droplet  multi-element airfoil  unstructured grid  two-phase flow  numerical simulation  
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