In-flight modal testing and analysis of a helicopter

被引：0
|
作者：
Hermans, L [1 ]
Van der Auweraer, H [1 ]
Hatami, A [1 ]
Cooper, JE [1 ]
Uhl, T [1 ]
Lisowski, W [1 ]
Wasilak, A [1 ]
机构：
[1] LMS Int, B-3001 Louvain, Belgium
来源：
IMAC - PROCEEDINGS OF THE 17TH INTERNATIONAL MODAL ANALYSIS CONFERENCE, VOLS I AND II | 1999年 / 3727卷
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：
This paper contains a preliminary report concerning the analysis of a data taken from the flight test of a helicopter. An overview of the Right test procedures is given followed by a discussion of the analysis approaches used. Some initial results obtained using ambient responses as the excitation source are given. Comparison is made with the results from the ground vibration test of the same helicopter.
引用
收藏
页码：80 / 86
页数：7
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