超空泡射弹尾拍振动特性分析
CSTR:
作者:
作者单位:

作者简介:

通讯作者:

中图分类号:

U661.1

基金项目:

国家自然科学基金资助项目(10802026)


Analysis of vibration characteristics of supercavitating projectiles under tail-slapping conditions
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:

    为了研究超空泡射弹的尾拍振动特性,利用刚-柔耦合动力学方法,得到弹体横向振动的基频和一阶模态;并通过模拟计算,分析了弹体横向振动基频和模态与弹体转速、长细比、材料特性的关系.计算结果表明:弹体频率和模态随转速而变化;弹体的长细比的增加和材料特性的改变,使频率和模态随转速的变化更加显著;当长细比较小或者角速度小于50 rad/s时,可以忽略耦合作用对振动的影响,频率可采用固有频率;当角速度小于100 rad/s时,可采用弹体的固有模态.

    Abstract:

    To study the vibration characteristics of supercavitating projectiles under tail-slapping conditions,the fundamental frequency and the first principal mode shape of the transverse vibration of projectiles were presented,based on the dynamics of coupling system for rigid and elastic motions.By simulations,the influences of rotational speed,slenderness ratio and material characteristics on frequency and the mode shape of vibration were investigated.The results show that the frequency and the mode shape vary with the rotational speed,and the increase of the slenderness ratio and the material characteristic parameter could accelerate these variations.For the small slenderness ratio or the rotational speed is less than 50 rad/s,the influence of coupled motions can be disregarded and the natural frequency can be used as the frequency of vibration,and the natural mode shape also can be used when the rotational speed is less than 100 rad/s.

    参考文献
    相似文献
    引证文献
引用本文

张劲生,张嘉钟,曹伟,魏英杰,于开平.超空泡射弹尾拍振动特性分析[J].哈尔滨工业大学学报,2011,43(11):16. DOI:10.11918/j. issn.0367-6234.2011.11.004

复制
相关视频

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:
  • 最后修改日期:
  • 录用日期:
  • 在线发布日期: 2012-04-26
  • 出版日期:
文章二维码