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两栖飞机入水冲击振动噪声特性数值仿真

徐佳伟 杭天一 梁泽豪 常道宾 胡世 李海超

中国舰船研究2025,Vol.20Issue(2):203-213,11.
中国舰船研究2025,Vol.20Issue(2):203-213,11.DOI:10.19693/j.issn.1673-3185.03479

两栖飞机入水冲击振动噪声特性数值仿真

Numerical simulation of vibration and noise characteristics of water entry impact of amphibious aircraft

徐佳伟 1杭天一 1梁泽豪 1常道宾 1胡世 1李海超1

作者信息

  • 1. 哈尔滨工程大学 船舶工程学院,黑龙江 哈尔滨 150001
  • 折叠

摘要

Abstract

[Objective]In response to the analysis requirements of the vibration and noise caused by the im-pact of amphibious aircraft entering the water,this paper studies the influence of forward speeds and entry angles on the water entry impact vibration and noise of amphibious aircraft.[Methods]First,based on the arbitrary Lagrangian-Eulerian(ALE)algorithm,a finite element model of an amphibious aircraft is estab-lished and its motion characteristics in the water entry impact stage under different forward speeds and water entry angles are analyzed.Next,based on the statistical energy snalysis(SEA)method,a SEA model of an am-phibious aircraft is established and its water entry impact vibration and noise characteristics are studied,as well as the influence of forward flight speed and entry angle.[Results]The results show that the lower the water forward speed,the smaller the response of the amphibious aircraft to the hydrodynamic impact,the less roll and the slower the longitudinal velocity decrease.The noise in the cockpit of the amphibious aircraft shows a trend of reducing across the entire frequency range.The effect of water entry angle on cockpit noise is not significant.Compared with other angles,the water entry angle of 4° has the greatest impact on the hydro-dynamic impact of the amphibious aircraft,but the best lateral stability.[Conclusion]By controlling the ap-propriate forward speed and water entry angle,the water entry attitude and cabin noise control can be taken in-to account.

关键词

两栖飞机/入水冲击/结构动力学/噪声/前飞速度/入水角度

Key words

amphibious aircraft/water impact/Structural dynamics/acoustic noise/forward speed/entry angle

分类

交通工程

引用本文复制引用

徐佳伟,杭天一,梁泽豪,常道宾,胡世,李海超..两栖飞机入水冲击振动噪声特性数值仿真[J].中国舰船研究,2025,20(2):203-213,11.

基金项目

国家自然科学基金资助项目(52101351,52371314) (52101351,52371314)

中国舰船研究

OA北大核心

1673-3185

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