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内埋弹舱舱门气动特性研究

吴继飞 徐来武 范召林 唐淋伟

空气动力学学报2012,Vol.30Issue(6):744-748,5.
空气动力学学报2012,Vol.30Issue(6):744-748,5.

内埋弹舱舱门气动特性研究

Investigation on aerodynamic characteristics of internal bay's door

吴继飞 1徐来武 2范召林 1唐淋伟1

作者信息

  • 1. 中国空气动力研究与发展中心,四川绵阳621000
  • 2. 空气动力学国家重点实验室,四川绵阳621000
  • 折叠

摘要

Abstract

An investigation on aerodynamic characteristics of internal weapons bay's door was conducted in high speed wind tunnel and the static/dynamic test results at Mach number equals to 0. 6 were presented in this paper. Static test results indicate that the acoustic noise around internal weapons bay's door is strong and the sound pressure level at the fore-edge of the door is close to the peak value of internal bay floor. Aerodynamic loads of the door change acutely with the variation of door's opening angle and that reach to the culmination when $ almost equals to 30? Dynamic test results show that aerodynamic loads of the door are influenced distinctly by St number. Aerodynamic characteristics have obvious difference between opening and closing process of the door.

关键词

内埋弹舱/气动噪声/声压级/气动载荷

Key words

internal bay/ acoustic noise/ sound pressure level (SPL)/ dynamic loads

分类

航空航天

引用本文复制引用

吴继飞,徐来武,范召林,唐淋伟..内埋弹舱舱门气动特性研究[J].空气动力学学报,2012,30(6):744-748,5.

空气动力学学报

OA北大核心CSCDCSTPCD

0258-1825

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