主管单位:中华人民共和国工业和信息化部
主办单位:西北工业大学  中国航空学会
地       址:西北工业大学友谊校区航空楼
伸缩机翼变体飞机气动特性研究
DOI:
作者:
作者单位:

第一飞机设计研究院,第一飞机设计研究院,第一飞机设计研究院

作者简介:

通讯作者:

中图分类号:

V221

基金项目:


The Aerodynamic Characteristics of Morphing Aircraft of Telescoping Wing
Author:
Affiliation:

The First Aircraft Institute,The First Aircraft Institute,The First Aircraft Institute

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    伸缩机翼变体飞机是通过机翼伸缩调整机翼展长,从而改变机翼面积和展弦比,改变飞机的气动布局和机翼的气动特性,满足多任务点的设计要求。本文简要介绍了伸缩机翼变体飞机的发展历史,重点研究了一种采用伸缩机翼设计的超音速飞机的气动特性变化。研究结果表明,亚音速时机翼展长伸长,展弦比增大,飞机诱导阻力降低,升阻比提高,可以明显提高飞机的航程;超音速时机翼展长缩短,展弦比减小,飞机的波阻降低,升阻比增大,提高了超音速飞行性能。伸缩机翼概念用于超音速飞机设计时能很好地兼顾亚音速巡航和超音速冲刺。

    Abstract:

    Morphing aircraft of telescoping wing can change wing area and aspect ratio by a variable-span morphing wing ,also change wing configuration and aerodynamic characteristics,which accommodate multiple flight conditions. This paper introduces in brief the development history of morphing aircraft of telescoping wing,and mainly explores the aerodynamic characteristics of a supersonic air vehicle with the concept of telescoping wing.The results of the analysis demonstrate an improvement in the aerodynamic characteristics of the morphing aircraft of telescoping wing.Wing span extension in subsonic represents a increase in aspect ratio and enhance the lift-drag ratio,in the form of a reduction in the induced drag,resulting in an increase in range.The wing span contraction represents a reduction in the aspect ratio and cut down the wave drag in supersonic,resulting in an increase in lift-drag ratio and improvement of flight performance of supersonic.Telescopic wing can take good consideration of both subsonic cruise and supersonic speed in supersonic aircraft design.

    参考文献
    相似文献
    引证文献
引用本文

李俊成,艾俊强,李士途.伸缩机翼变体飞机气动特性研究[J].航空工程进展,2013,4(1):22-27

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2012-12-03
  • 最后修改日期:2013-01-05
  • 录用日期:2013-01-07
  • 在线发布日期: 2013-10-22
  • 出版日期: