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高超音速飞行器气动热研究进展

陈雄昕 刘卫华 罗智胜 赵宏韬 冯诗愚

航空兵器Issue(6):8-13,6.
航空兵器Issue(6):8-13,6.

高超音速飞行器气动热研究进展

Research Advan ces of Aerodynamic Heating for Hypersonic Aircraft

陈雄昕 1刘卫华 1罗智胜 2赵宏韬 2冯诗愚1

作者信息

  • 1. 南京航空航天大学,南京 210016
  • 2. 中航工业合肥江航飞机装备有限公司,合肥 230051
  • 折叠

摘要

Abstract

Due to the unparallel advantage of the hypersonic vehicles compared with the common su-personic ones, it becomes the important development direction in the area of the aeronautics and astronau-tics.However , this technology is dramatically restricted by the violent aerodynamic heating which is caused by the ultra-high speed viscous flow of air through the aircraft surfaces and will affect the security of aircrafts.Obviously, it is the key technology for the design of hypersonic aircrafts to comprehend the change rules of the aerodynamic heating.The current research results and prospective on the aerodynamic heating for hypersonic aircrafts are summarized including experiments and numerical simulations.

关键词

高超音速/气动加热/数值模拟/工程算法

Key words

hypersonic/aerodynamic heating/numerical simulation/engineering algorithm

分类

航空航天

引用本文复制引用

陈雄昕,刘卫华,罗智胜,赵宏韬,冯诗愚..高超音速飞行器气动热研究进展[J].航空兵器,2014,(6):8-13,6.

基金项目

航空科学基金资助项目 ()

航空兵器

OACSTPCD

1673-5048

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