Three-dimensional numerical simulation of rime ice accretions on an aircraft wing

ZHANG Qiang; CAO Yi-hua; ZHONG Guo

Chinese

您当前的位置：

首页 >

文章列表页 >

Three-dimensional numerical simulation of rime ice accretions on an aircraft wing

更新时间：2026-07-07

- Three-dimensional numerical simulation of rime ice accretions on an aircraft wing
- Vol. 25, Issue 6, (2010)
- 作者机构：
  
  北京航空航天大学航空科学与工程学院,北京,100191
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2010
- 稿件说明：
移动端阅览
ZHANG Qiang, CAO Yi-hua, ZHONG Guo. Three-dimensional numerical simulation of rime ice accretions on an aircraft wing[J]. 2010, 25(6).
DOI：

ZHANG Qiang, CAO Yi-hua, ZHONG Guo. Three-dimensional numerical simulation of rime ice accretions on an aircraft wing[J]. 2010, 25(6). DOI：

摘要

基于欧拉两相流理论对三维情况下飞机机翼表面的霜冰进行了数值模拟.根据水滴拟流体模型建立三维水滴控制方程;提出一套水滴控制方程的数值求解方法;由三维水滴流场的求解结果计算机翼表面的水滴收集特性

提出一种三维积冰外形的生成方法

完成了对飞机机翼表面霜冰的三维数值模拟.对ONERA M6机翼在不同迎角下霜冰的积冰情况进行了数值预测

并分析了结冰条件对积冰的影响.

Abstract

Based on Eulerian two-phase flow theory

the rime ice accretions on an aircraft wing in three-dimensional application were numerically simulated.The governing equations for droplets in three-dimensional application were established according to the droplet pseudo-fluid model.A set of numerical methods for solving the droplet governing equations were proposed.The local collection efficiency and impingement area on the wing were computed from the solution of the three-dimensional droplet flowfield.A method of building three-dimensional ice accretion shape was proposed.The rime ice accretions on an ONERA M6 wing under different angles of attack were predicted numerically and the effects of icing conditions on the ice accretion were analyzed.

关键词

Keywords

references

Views

513

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Three-dimensional numerical simulation of supercooled droplets impinging on a wing

Numerical simulation of ice accretions on multi-element airfoils

Application of unstructured grids in numerically simulating ice accretions

Numerical simulation of glaze ice accretions on an airfoil

Simulation method of short crack propagation in turbine disks based on crystal plasticity

Related Author

HU Li

ZHANG Qiang

GAO Zheng-hong

FU Lin

Ping ZHANG

Shan LU

Xin JING

Mao YANG

Related Institution

National Key Laboratory of Science and Technology on Aerodynamic Design and Research, School of Aeronautics, Northwestern Polytechnical University

School of Power and Energy，Northwestern Polytechnical University

Nondestructive Testing and Evaluation Laboratory， Dalian University of Technology

College of Civil Engineering， Hefei University of Technology

Key Laboratory of Aerospace Chemical Power Technology， Hubei Institute of Aerospace Chemical Techologh， China Aerospace Science and Technology Corporation，Xiangyang Hubei

AI问答

Postal code：100079
Tel：（010）53879206 Email：tmw@bjxintong.com.cn
Technical support is provided by Beijing Founder electronics co., LTD 京ICP备09082226号-64 京公网安备11010602201714号
It is recommended to read the content of this site in Chrome&IE9+. Please switch to extreme mode in browser 360.
Cookies We use cookies to help provide and enhance our service and tailor content. By continuing, you agree to the use of cookies.

⁰