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全机颤振风洞试验模型地面共振试验影响因素分析

赵冬强 胡志勇 高宏

航空科学技术Issue(7):61-65,5.
航空科学技术Issue(7):61-65,5.

全机颤振风洞试验模型地面共振试验影响因素分析

Affecting Factors Analysis of GVT for Aircraft Flutter Wind Tunnel Model

赵冬强 1胡志勇 1高宏1

作者信息

  • 1. 中航工业第一飞机设计研究院,陕西 西安 710089
  • 折叠

摘要

Abstract

In order to exclude the affecting factors on the Ground Vibration Test(GVT) and improve the precision of the test result, the numerical simulation model was established, and the affection of the suspension stiffness, sensor, and drive rod was studied. The result shows that the larger the suspension stiffness is, the stronger the inlfuence wil be. Sensor’s added mass mostly inlfuences the control surface’ rotation frequency. The more the sensors are, the smaler the test frequency wil be. In addition, the drive rod’s added stiffness wil improve some modes’ test frequencies.

关键词

全机颤振风洞试验模型/地面共振试验/影响因素/悬挂刚度/传感器/激振杆

Key words

aircraft flutter wind tunnel model/ground vibration test(GVT)/affecting factor/suspension stiffness/sensor/drive rod

分类

航空航天

引用本文复制引用

赵冬强,胡志勇,高宏..全机颤振风洞试验模型地面共振试验影响因素分析[J].航空科学技术,2015,(7):61-65,5.

航空科学技术

1007-5453

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