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四分量片式铰链力矩天平技术及风洞实验应用研究

刘喜贺 王天昊 邱俊文 李盛文 冯昕华

实验流体力学2011,Vol.25Issue(2):88-91,4.
实验流体力学2011,Vol.25Issue(2):88-91,4.

四分量片式铰链力矩天平技术及风洞实验应用研究

Hinge moment balance technique with axial force measurement and its application in wind tunnel test

刘喜贺 1王天昊 1邱俊文 1李盛文 1冯昕华1

作者信息

  • 1. 中国航空工业空气动力研究院,哈尔滨150001
  • 折叠

摘要

Abstract

For resolve the non-axial force measurement limitations of three-component hinge moment balance on wind tunnel control flap test, a operable design plan of four-component hinge moment balance is put forward in this paper, then a physical prototype was application in the elevator experiment. The result shows that the experiment result and theoretical analysis have good consistency when elevator angle is 21 degree, normal force coefficient relative error is 14.7% and control flap's pressure center position relative error is 20 %, which ignore the axial force measurement.

关键词

铰链力矩天平/轴向力元件/舵面法向力系数/舵面压心位置/风洞实验

Key words

hinge moment balance / axial force measurement/ normal force coefficient / pressure center position/wind tunnel test

分类

机械制造

引用本文复制引用

刘喜贺,王天昊,邱俊文,李盛文,冯昕华..四分量片式铰链力矩天平技术及风洞实验应用研究[J].实验流体力学,2011,25(2):88-91,4.

基金项目

航空科学基金(2009ZD27005) (2009ZD27005)

实验流体力学

OA北大核心CSCDCSTPCD

1672-9897

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