Computational Modeling of Helicopter Loading Processes during Splashdown in Dynamic Statement

被引:0
|
作者
Gontsova L.G. [1 ]
Nedel’ko D.V. [1 ]
Safiullin A.F. [2 ]
机构
[1] Central Aerohydrodynamic Institute (TsAGI), ul. Zhukovskogo 1, Zhukovsky
[2] PAO Kazan Helicopters, ul. Tetsevskaya 14, Tatarstan, Kazan
来源
Russian Aeronautics | 2023年 / 66卷 / 3期
关键词
emergency splashdown system; finite element method; helicopter splashdown;
D O I
10.3103/S1068799823030261
中图分类号
学科分类号
摘要
Abstract: The experience of using a set of programs that implement the finite element method to determine overloads during the splashdown process of a helicopter with and without installed emergency splashdown system, is considered. The calculation results are compared with experimental data in order to determine the applicability of the finite element method in solving problems of hydrodynamic loading of a helicopter. © 2023, Allerton Press, Inc.
引用
收藏
页码:625 / 631
页数:6
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