基于乘波构形的跨大气层飞行器气动布局
DOI:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:

国家自然科学基金项目(10502056)


Aerodynamic Configuration of Trans-atmospheric VehicleBased on Waverider Research
Author:
Affiliation:

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:

    利用乘波构形具有升阻比大的特点,将其作为滑翔跳跃式跨大气层飞行器的基准外形进行研究,提出了乘波构形的设计方法,详细分析了各设计参数对乘波构形的影响,研究了不同马赫数、不同优化目标下得到的乘波体的性能,得到了升阻比大、容积效率高的跨大气层飞行器气动布局,所得结论对跨大气层飞行器气动布局和乘波体外形的研究具有一定的参考价值。

    Abstract:

    This article researched the aerodynamic configuration design of the glide/skip trans-atmospheric vehicle(TAV) based on waverider with high lift-to-drag ratio. Firstly, design methods of waverider configuration were put forward, and the waverider shape changed from design parameters was fully investigated. Then, the performances of the optimized waveriders under the varieties of Mach number and differed optimization aims were compared and studied. Finally, a TAV configuration with high L-D ratio and high volumetric efficiency was obtained. The conclusion has important reference value to the research of TAV configuration and waverider.

    参考文献
    相似文献
    引证文献
引用本文

何烈堂,周伯昭,陈磊.基于乘波构形的跨大气层飞行器气动布局[J].国防科技大学学报,2007,29(4):17-21.
HE Lietang, ZHOU Bozhao, CHEN Lei. Aerodynamic Configuration of Trans-atmospheric VehicleBased on Waverider Research[J]. Journal of National University of Defense Technology,2007,29(4):17-21.

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:2006-11-03
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2013-02-28
  • 出版日期:
文章二维码