冰形表面粗糙度对翼型的失速特性影响分析

黄冉冉; 李栋; 刘藤; 丁钰良

doi:10.7638/kqdlxxb-2019.0046

欢迎来到能源电力期刊网！

English Version 期刊登录

您当前的位置：

首页 >

文章列表页 >

冰形表面粗糙度对翼型的失速特性影响分析

研究论文 | 更新时间：2026-05-28

- 冰形表面粗糙度对翼型的失速特性影响分析
- The effect of ice accretion roughness on airfoil stall characteristics
- 空气动力学学报 2021年39卷第1期页码：59-65
- 作者机构：
  
  1. 西北工业大学,西安,710072
  2. 中国飞行试验研究院,西安,710089
- 作者简介：
  
  黄冉冉(1995-), 女, 江西人, 硕士, 研究方向: 飞机容冰设计.E-mail: ranran@mail.nwpu.edu.cn
  李栋(1970-), 男, 教授, 研究方向: 计算流体力学, 设计空气动力学.E-mail: ldgh@nwpu.edu.cn
- 基金信息：
- DOI：10.7638/kqdlxxb-2019.0046
  中图分类号： V211.3
- 纸质出版：2021
- 稿件说明：
移动端阅览
黄冉冉, 李栋, 刘藤, 丁钰良. 冰形表面粗糙度对翼型的失速特性影响分析[J]. 空气动力学学报, 2021, 39(1): 59-65.

HUANG Ranran, LI Dong, LIU Teng, et al. The effect of ice accretion roughness on airfoil stall characteristics[J]. 2021, 39(1): 59-65.
黄冉冉, 李栋, 刘藤, 丁钰良. 冰形表面粗糙度对翼型的失速特性影响分析[J]. 空气动力学学报, 2021, 39(1): 59-65. DOI： 10.7638/kqdlxxb-2019.0046.

HUANG Ranran, LI Dong, LIU Teng, et al. The effect of ice accretion roughness on airfoil stall characteristics[J]. 2021, 39(1): 59-65. DOI： 10.7638/kqdlxxb-2019.0046.

摘要

结冰翼型气动影响分析是飞机结冰问题重要的研究内容之一，可帮助进行飞机结冰安全分析和容冰设计。为填补现阶段关于冰形表面粗糙度对翼型气动影响的研究空缺，以冰形的粗糙度参数（冰形表面粗糙高度和冰形表面粗糙分散度）为依据，提出了一种冰形粗糙度叠加方法；并通过有限体积法求解空间离散的RANS方程，结合S-A湍流模型，分别针对流线冰型和角状冰型，量化分析了不同微观特征参数的冰形对翼型失速特性的影响规律，为研究飞机结冰问题提供了思路和基础。结果表明，对于流线结冰翼型，冰形表面粗糙度会明显影响翼型的失速性能；而对于角状结冰翼型，两个凸起的羊角状外形才是导致气动力损失的主要因素，粗糙度的影响往往可不考虑在内。

Abstract

The aerodynamic impact of ice accretion is one of the most important research contents in aircraft icing problems. However

to the authors' knowledge

related studies on the effect of ice roughness on airfoil aerodynamic characteristics are still quite rare. Therefore

the present paper proposes an ice roughness superposition method based on ice roughness parameters (surface roughness height and surface roughness dispersion). The Reynolds averaged Navier-Stokes equations are solved by the finite volume method with the S-A turbulence model. The influence of ice accretion with different ice roughness parameters on airfoil aerodynamic characteristics

especially on the airfoil stall characteristics

is analyzed for both rime ice and glaze ice

which will hopefully provides some enlightenment for aircraft icing problems. Results show that

the roughness parameters of the rime ice will result in a significant effect on airfoil stall performance. However

for a glaze iced airfoil

the two horn-like protrusions are the main factors causing the aerodynamic loss

while the effect of ice roughness parameters is negligible.

关键词

Keywords

references

YI X. Numerical computation of aircraft icing and study on icing test scaling law[D]. Mianyang: China Aerodynamics Research and Development Center, 2007, 12. (in Chinese)

CEBECI T, KAFYEKE F. Aircraft icing[J]. Annual Review of Fluid Mechanics, 2003, 35(35): 11-21.

BRAGG M B, BROEREN A P, BLUMENTHAL L A. Iced-airfoil aerodynamics[J]. Progress in Aerospace Sciences, 2005, 41(5): 323-362.

LEE S, BRAGG M. Effects of simulated-spanwise-ice shapes on airfoils-experimental investigation[C]//Aerospace Sciences Meeting Exhibit. 2013.

DUNN T A, LOTH E, BRAGG M B. Computational investigation of simulated large-droplet ice shapes on airfoil aerodynamics[J]. Journal of Aircraft, 1999, 36(5): 836-843.

CHUNG J, REEHORST A, CHOO Y, et al. Navier-Stokes analysis of flowfield characteristics of an ice-contaminated aircraft wing[J]. Journal of Aircraft, 2000, 37(6): 947-959.

PAN J, LOTH E. Reynolds-averaged Navier-Stokes simulations of airfoils and wings with ice shapes[J]. Journal of Aircraft, 2004, 41(4): 879-891.

LEE S, BRAGG M B. Experimental investigation of simulated large-droplet ice shapes on airfoil aerodynamics[J]. Journal of Aircraft, 1999, 36(5): 844-850.

ZHU D Y, ZHANG F K, ZHOU Z H, et al. Research on critical ice shape determination and its effects on aerodynamics[J]. Acta Aerodynamic Sinica, 2016, 34(6): 714-720. (in Chinese)

ANDERSON D N, HENTSCHEL D B, RUFF G A. Measurement and correlation of ice accretion roughness[C]//36th AIAA Aerospace Sciences Meeting and Exhibit. Reno, NV: AIAA, 1998.

FORTIN G, ILINCA A, LAFORTE J L, et al. New roughness computation method and geometric accretion model for airfoil icing[J]. Journal of Aircraft, 2004, 41(1): 119-127.

CHANG S N, LI Y, HUO X H. Analysis and modeling of aircraft icing surface roughness[C]//CCTAM. ZhengZhou: CSTAM, 2009. (in Chinese)

SHIN J. Characteristics of surface roughness associated with leading-edge ice accretion[J]. Journal of Aircraft, 2015, 33(2): 316-321.

BRAGG M, CUMMINGS M, HENZE C. Boundary-layer and heat-transfer measurements on an airfoil with simulated ice roughness[C]//Aerospace Sciences Meeting Exhibit. 1996.

BRAGG M B, BROEREN A P, BLUMENTHAL L A. Iced-airfoil aerodynamics[J]. Progress in Aerospace Sciences, 2005, 41(5): 323-362.

MATHEIS. Numerical investigation of roughness effects in aircraft icing calculations[D]. Iowa State University, 2008.

LI H T, SHU LC, HU Q, et al. Numerical simulation of wind turbine blades aerodynamic performance based on ice roughness effect[J]. Transactions of China Electrotechnical Society, 2018, 33(10): 2253-2260. (in Chinese)

CHI X, LI Y, CHEN H, et al. A comparative study using CFD to predict iced airfoil aerodynamics[C]//AIAA Aerospace Sciences Meeting Exhibit. Reno. NV: AIAA, 2005.

CHUNG J J, ADDY H E. A numerical evaluation of icing effects on a natural laminar flow airfoil[C]//38th Aerospace Sciences Meeting. Reno, NV: AIAA, 2000.

GURBACKI H M. Ice-induced unsteady flow field effects on airfoil performance[D]. Urbana, IL: Univ. of Illinois at Urbana-Champaign, 2003.

浏览量

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

离心通风机降噪研究进展

基于神经网络与遗传算法的热气防冰结构优化

大展弦比飞行器突风响应数值计算

基于Ac-准则的最优输入设计方法

水滴撞击运动超疏水表面特性及其调控