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飞机热气防冰系统与冰脊预测的数值模拟

王昆 白俊强 夏露 李鑫 马献伟

王昆, 白俊强, 夏露, 李鑫, 马献伟. 飞机热气防冰系统与冰脊预测的数值模拟[J]. 航空动力学报, 2014, 29(11): 2694-2703. doi: 10.13224/j.cnki.jasp.2014.11.021
引用本文: 王昆, 白俊强, 夏露, 李鑫, 马献伟. 飞机热气防冰系统与冰脊预测的数值模拟[J]. 航空动力学报, 2014, 29(11): 2694-2703. doi: 10.13224/j.cnki.jasp.2014.11.021
WANG Kun, BAI Jun-qiang, XIA Lu, LI Xin, MA Xian-wei. Numerical simulation of aircraft hot air anti-icing system and ice ridge prediction[J]. Journal of Aerospace Power, 2014, 29(11): 2694-2703. doi: 10.13224/j.cnki.jasp.2014.11.021
Citation: WANG Kun, BAI Jun-qiang, XIA Lu, LI Xin, MA Xian-wei. Numerical simulation of aircraft hot air anti-icing system and ice ridge prediction[J]. Journal of Aerospace Power, 2014, 29(11): 2694-2703. doi: 10.13224/j.cnki.jasp.2014.11.021

飞机热气防冰系统与冰脊预测的数值模拟

doi: 10.13224/j.cnki.jasp.2014.11.021
详细信息
    作者简介:

    王昆(1988-),男,四川内江人,硕士生,主要从事计算流体力学、飞机积冰及防除冰技术研究.

  • 中图分类号: V211

Numerical simulation of aircraft hot air anti-icing system and ice ridge prediction

  • 摘要: 基于流固耦合传热的思想建立了一套飞机热气防冰系统的的数值模拟方法,并将其与积冰热力学模型结合起来,实现了热气防冰系统开启时的机翼积冰预测.采用格心格式有限体积法求解N-S方程获得防冰腔与外流场;通过欧拉法在外流场的基础上获得过冷水滴撞击特性;求解三维热传导偏微分方程获得蒙皮的传热特性;采用交接面插值的方法实现防冰腔到外流场的热量传递;建立了考虑三维溢流效应的积冰热力学模型并在此基础上开展了机翼冰脊的数值预测.数值模拟结果表明:热气防冰系统开启时加热机翼表面温度最高可达308K,加热区后的上下机翼表面均有冰脊形成,通过对结果的分析表明该方法是合理可行的.

     

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出版历程
  • 收稿日期:  2013-07-12
  • 刊出日期:  2014-11-28

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