Modeling, experimental research and critical parameter analysis of glider's dynamic characteristics

被引：0
|
作者：
Rugaitis, A. [1 ]
Juocas, K. [2 ]
Volkovas, V. [3 ]
Deksnys, V. [1 ]
机构：
[1] Kaunas Univ Technol, LT-51368 Kaunas, Lithuania
[2] Sportine Aviacija Ir Ko, LT-59327 Pociunai, Prienai, Lithuania
[3] Kaunas Univ Technol, LT-44312 Kaunas, Lithuania
来源：
MECHANIKA | 2010年 / 06期
关键词：
D O I：
暂无
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The work studies results of glider dynamical characteristics modeling and ground tests. It presents a methodology of defining natural frequencies of glider structure and parameters characterizing flutter phenomenon, analysis of developed means designated for performance of glider ground frequency tests. The paper presents results of modeling of resonant frequencies of LAK-17B glider structural elements, which are compared to experimental results of ground dynamical tests. The efficiency of application of the demonstrated methodology allows defining possible flutter phenomena of structural elements of the mentioned glider and their vibration decrements.
引用
收藏
页码：38 / 42
页数：5
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