江苏科技信息 ›› 2016, Vol. 33 ›› Issue (8): 57-59.doi: 10.3969/j.issn.1004-7530.2016.08.023

• 论文 • 上一篇    下一篇

鸭翼布局飞行动力学特性及发展现状

李中华, 田会杰, 徐东明   

  1. 上海飞机设计研究院,上海,200120
  • 出版日期:2016-03-15 发布日期:2016-03-15

Flight Dynamics Characteristics and Current Situation of Canard Aircraft

Li Zhonghua, Tian Huijie, Xu Dongming   

  • Online:2016-03-15 Published:2016-03-15

摘要: 文章简要介绍了鸭翼布局飞机的发展历程及几何特性,回顾了近年来所做的代表性研究,分析了鸭翼布局的主要动力学特性,展示了当今应用的现状及未来发展方向。

关键词: 飞行动力学, 大迎角, 升阻比

Abstract: This article briefly introduces the geometry property and the history of the canard aircraft; and then we review the representative studies on canard configuration done in recently years. The article analyzes main aerodynamic characteristics of canard configuration and presens advanced canard aircraft in the world and the future developing trend of canard configuration.