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2.4m跨声速风洞多功能支撑系统试验技术研究

陈德华 刘大伟 尹陆平 师建元 彭超 饶正周

实验流体力学2013,Vol.27Issue(3):98-102,112,6.
实验流体力学2013,Vol.27Issue(3):98-102,112,6.

2.4m跨声速风洞多功能支撑系统试验技术研究

The study of versatile support system in the 2.4m transonic wind tunnel

陈德华 1刘大伟 2尹陆平 1师建元 2彭超 2饶正周2

作者信息

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

摘要

Abstract

A test technique research for versatile support system was conducted in the 2.4 meter transonic wind tunnel.Applying this system in wind tunnel test could be implemented in a manner of continuously changing sideslip angle at a constant attack angle besides continuously changing attack angle at a constant sideslip angle.Introductory investigation on versatile support system was conducted in 0.6 meter transonic wind tunnel.Test applying for the versatile support system in comparison with traditional system was conducted in the 2.4 meter transonic wind tunnel.Results indicated that test data obtained with two different support systems presented a good correlation,and the design of versatile support system was successful.

关键词

跨声速风洞/多功能支撑系统/试验技术/试验效率

Key words

transonic wind tunnel/versatile support system/ test technique/test efficiency

分类

航空航天

引用本文复制引用

陈德华,刘大伟,尹陆平,师建元,彭超,饶正周..2.4m跨声速风洞多功能支撑系统试验技术研究[J].实验流体力学,2013,27(3):98-102,112,6.

基金项目

空气动力学国家重点实验室(11010205) (11010205)

实验流体力学

OA北大核心CSCDCSTPCD

1672-9897

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