A flight test to demonstrate flutter and evaluate the flutterometer

被引:1
|
作者
Lind, R [1 ]
Voracek, DF
Truax, R
Doyle, T
Potter, S
Brenner, M
机构
[1] Univ Florida, Dept Aerosp Engn, Gainesville, FL 32611 USA
[2] NASA, Dryden Flight Res Ctr, Edwards AFB, CA USA
来源
AERONAUTICAL JOURNAL | 2003年 / 107卷 / 1076期
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A project was recently completed that investigated the ability to predict the onset of flutter using tools like the flutterometer. This project used an experiment called the aerostructures test wing that was flown while mounted to the flight test fixture on an F-15. Several flight tests were conducted to expand the envelope and determine he aeroelastic dynamics of the experiment. The final flight ended with destruction of the experiment due to the onset of flutter. The flutterometer attempted to predict this onset by analysing the flight data. The results indicate the flutterometer is able to generate a conservative estimate of the flight conditions associated with flutter. This paper details the flight tests of the experiment and the resulting predictions from the flutterometer.
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页码:577 / 588
页数:12
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