超空泡航行体双层壳结构动力稳定性分析
DOI:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

基金项目:


Dynamic Stability Analysis of Supercavitating Double Shells
Author:
Affiliation:

Fund Project:

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    针对超空泡航行体轴向受力特点,建立超空泡航行体双层壳结构有限元模型,对结构动力稳定性进行分析。数值计算表明,当壳间实肋板厚度增大或环向 肋骨数量和尺寸增加时,动力失稳区域整体下移,不稳定激发频率下降,失稳区域宽度减小幅度较小;当壳间间距减小或纵向肋骨数量和尺寸增加时,双层壳结构动力不稳定激发频率上升,动力失稳区域宽度较大幅度减小,动力不稳定激发程度显著降低。

    Abstract:

    A finite element model for supercavitating underwater vehicles was developed and the dynamic stability of supercavitating double shells was investigated to obtain the instability maps for varying vehicle's velocity considering the time-dependent properties of the longitudinal loads. The computational results indicate that with the increment of the thickness of the annular plates linking between inner and outer shells or the number and dimension of the circumferential stiffeners, the frequencies corresponding to dynamic instability decline and the extension of the regions of dynamic instability is reduced lightly, while the frequencies corresponding to dynamic instability ascend and the dynamic stability is enhanced remarkably with the space between inner and outer shells decreased or the number and dimension of the longitudinal stiffeners increased.

    参考文献
    相似文献
    引证文献
引用本文

麻震宇,胡凡,陈广南,等.超空泡航行体双层壳结构动力稳定性分析[J].国防科技大学学报,2011,33(4):43-47.
MA Zhenyu, HU Fan, CHEN Guangnan, et al. Dynamic Stability Analysis of Supercavitating Double Shells[J]. Journal of National University of Defense Technology,2011,33(4):43-47.

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2011-04-13
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2012-08-28
  • 出版日期:
文章二维码