首页 | 本学科首页   官方微博 | 高级检索  
     

水下航行体舱段结构声学设计模型分析
引用本文:艾海峰, 陈志坚, 王路. 水下航行体舱段结构声学设计模型分析[J]. 中国舰船研究, 2010, 5(6): 12-15. DOI: 10.3969/j.issn.1673-3185.2010.06.003
作者姓名:艾海峰  陈志坚  王路
作者单位:1.[1]海军工程大学船舶与动力学院,湖北武汉430033 [2]海军装备研究院舰船论证研究所,北京100161
基金项目:国防"十一五"预研项目
摘    要:采用基于模态坐标的有限元/边界元方法,建立水下航行体封闭舱段声学设计模型,利用该耦合分析模型对两端采用刚性圆板封闭的简支舱段结构的振声性能进行分析,并与采用半无限长圆柱形刚性障板代替两端的刚性圆板时的舱段模型计算结果作比较,指出除了少数耦合模态的固有频率附近,当外层圆柱壳周长相对流体中声波波长较小时,采用刚性圆板封闭的两端简支双层加筋圆柱壳与两端采用半无限长圆柱形刚性障板代替刚性圆板时的声辐射规律十分相近。

关 键 词:舱段  有限元/边界元  双层加筋圆柱壳  声辐射
收稿时间:2010-04-09
修稿时间:2010-05-29

Structural-Acoustic Analysis on the Cabin of Underwater Vehicle
Ai Haifeng, Chen Zhijian, Wang Lu. Structural-Acoustic Analysis on the Cabin of Underwater Vehicle[J]. Chinese Journal of Ship Research, 2010, 5(6): 12-15. DOI: 10.3969/j.issn.1673-3185.2010.06.003
Authors:Ai Hai-feng  Chen Zhi-jian  Wang Lu
Affiliation:1 College of Naval Architecture and Power,Naval University of Engineering,Wuhan 430033,China; 2 The Institute of Naval Vessel,Naval Academy of Armament,Beijing 100161,China )
Abstract:The structural-acoustic design model for an enclosed cabin section of underwater vehicle was built up using FEM/BEM method based on modal coordinates,the vibration and sound radiation characteristics were analyzed by this coupled design model for the simple supported finite cylindrical shell ended with rigid circular plates.The results were compared with that of substituting semi-infinite rigid cylindrical baffles for the rigid circular plates.It demonstrates that as the perimeter of the outer cylindrical shell is smaller compared to the wavelength of sound in ambient fluid,the sound radiation law of the simple supported and stiffened double cylindrical shell ended with rigid circular plates is similar with that extended by two semi-infinite length rigid cylindrical baffles,except the case that is near the natural frequencies of a few coupled modes.
Keywords:cabin  FEM/BEM  stiffened double cylindrical shell  sound radiation
本文献已被 维普 万方数据 等数据库收录!
点击此处可从《中国舰船研究》浏览原始摘要信息
点击此处可从《中国舰船研究》下载全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号