Overview of several ice accretion effects on aircraft flight dynamics

SU Yuan; XU Zhong-da; WU Zhen-long

doi:10.13224/j.cnki.jasp.2014.08.017

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Overview of several ice accretion effects on aircraft flight dynamics

更新时间：2026-07-07

- Overview of several ice accretion effects on aircraft flight dynamics
- Issue 8, (2014)
- 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：10.13224/j.cnki.jasp.2014.08.017
  CLC：
- Published：2014
- 稿件说明：
移动端阅览
苏媛, 徐忠达, 吴祯龙. 飞机积冰后若干飞行力学问题综述[J]. 航空动力学报, 2014, (8): 1878-1893. doi: 10.13224/j.cnki.jasp.2014.08.017

SU Yuan, XU Zhong-da, WU Zhen-long. Overview of several ice accretion effects on aircraft flight dynamics[J]. 2014, (8).
苏媛, 徐忠达, 吴祯龙. 飞机积冰后若干飞行力学问题综述[J]. 航空动力学报, 2014, (8): 1878-1893. doi: 10.13224/j.cnki.jasp.2014.08.017 DOI：

SU Yuan, XU Zhong-da, WU Zhen-long. Overview of several ice accretion effects on aircraft flight dynamics[J]. 2014, (8). DOI： 10.13224/j.cnki.jasp.2014.08.017.

摘要

回顾飞机积冰后若干飞行力学问题研究的历史与现状，着重介绍了积冰飞机气动数据的获取途径、积冰飞机飞行力学建模与飞行仿真、积冰对飞机稳定性和操纵性的影响以及积冰对飞机飞行性能的影响.在已有飞机积冰后飞行力学问题研究的基础上，提出了飞机积冰后飞行力学问题研究领域需要解决和关注的若干问题，包括通过数值模拟方法获取积冰飞机的气动数据、完善积冰对飞机气动导数影响的计算模型以及加强平尾失速方面的研究.今后需要进一步对模拟冰风洞、数值模拟方法和平尾失速进行研究，并获取更多实验数据.

Abstract

An overview of the studies about several ice accretion effects on aircraft flight dynamics was presented here. Special attention was paid to the following areas: the way to obtain the aerodynamic data of iced aircraft

the flight dynamic modeling and simulation of iced aircraft

the effect of ice accretion on the stability and handling quality characteristics as well as the flight performance. Based on the progress of existing research in these areas

some key issues deserving more attention of the researchers for resolution are addressed

including: obtaining the aerodynamic data of iced aircraft through numerical simulation method

consummating the calculation model of effects of ice accretion on aircraft aerodynamic derivatives and enhancing the investigation on stall problems of tailplane. The simulated ice wind tunnel

numerical simulation method

stall of tailplane should be further studied and more test data should be obtained in the future.

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