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弹箭与制导学报 >

2014 , Vol. 34 >Issue 3: 129 - 132

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2014.03.024

弹道与气动力技术

海浪对巡航导弹掠海飞行气动性能的影响

  • 李妍 ,
  • 陈希 ,
  • 费树岷
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  • 1 东南大学自动化学院, 南京 210098
    2 解放军理工大学气象海洋学院, 南京 211101

李妍(1974-),女,辽宁本溪人,副教授,研究方向:大气海洋环境信息智能化处理以及环境对武器装备效能影响等。

收稿日期: 2013-06-19

  网络出版日期: 2025-05-30

基金资助

国家自然科学基金(60835001)

收起

The Research on Influence of Wave on Pneumatic Performance of Sea-skimming Cruise Missile

  • LI Yan ,
  • CHEN Xi ,
  • FEI Shumin
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  • 1 School of Automation, Southeast University, Nanjing 210098, China
    2 Institute of Meteorology and Ocean, PLA University of Science and Technology, Nanjing 211101, China

Received date: 2013-06-19

  Online published: 2025-05-30

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摘要

文中在导弹的动力学模型中考虑了海浪要素的影响,客观定量分析了海浪对巡航导弹掠海飞行的影响。首先,利用第三代近岸海浪数值计算模式进行随机海浪的计算,提取海浪的能量谱分布;然后,建立以巡航导弹为中心的运动坐标系,计算出运动坐标系下的海浪谱;在此基础上,计算了浪致风场;最后,将海浪导致的风场引入导弹的气动参数计算中,并进行了仿真试验,结果表明该方法实用性强、效果好。

关键词： 巡航导弹; 掠海飞行; 海浪; 气动性能

本文引用格式

李妍 , 陈希 , 费树岷 . 海浪对巡航导弹掠海飞行气动性能的影响[J]. 弹箭与制导学报, 2014 , 34(3) : 129 -132 . DOI: 10.15892/j.cnki.djzdxb.2014.03.024

Abstract

The influence of wave was considered for kinetic model of missile, and the influence of wave on sea-skimming of cruise missile was analyzed objectively and quantitatively. At first, the ocean wave was simulated by energy spectral from simulation wave ashore near (SWAN) model. Then, moving energy spectral was concluded in moving coordinates. On the base of above, wave induced wind was computed according to the correlation between wave and wind over sea. At last, wave induced wind was introduced into missile kinetic function, and applied to simulation; Results show that our method is feasible and very practicable.

Key words： cruise-missile; sea-skimming; wave; pneumatic capability

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参考文献

[1]
史和生, 王耀华, 许漪. 能实现多点攻击的巡航导弹指挥模型研究[J]. 战术导弹控制技术, 2005, 31(3): 95-99.
[2]
党宏涛, 张胜修. 巡航导弹跨海飞行高度跟踪系统仿真[J]. 弹箭与制导学报, 2006, 26(3): 32-34.
[3]
廖朝晖摘译. 各种海情下低空飞行的导弹分析[J]. 飞航导弹, 1992 (11): 2-9.
[4]
秦志强, 王明海, 湛必胜. 巡航导弹海上生存能力模型研究[J]. 弹箭与制导学报, 2006, 26(3): 71-73.
[5]
雷小龙, 关世义, 常伯浚. 掠海飞行导弹击水概率的仿真研究[J]. 宇航学报, 1990 (3): 16-21.
[6]
湛必胜, 王明海, 李邦杰, 等. 巡航导弹飞行撞地概率的一种计算方法[J]. 飞行力学, 2006, 24(3): 78-80.
[7]
Phillips O M. On the generation of waves by turbulent wind[J]. J. Fluid Mech., 1957, 2(5): 417-445.
[8]
Miles, J W. On the generation of surface waves by shear flows[J]. J. Fluid Mech., 1957, 3(2): 185-204.
[9]
文圣常, 余宙文. 海浪理论与计算原理[M]. 北京: 北京科学出版社, 1984:127-249.
[10]
Holthuijsen LH, et al. SWAN Cycle III version 40.72ABCD user manual[M]. Delft University of Technology, 2009.
[11]
Venas B, Satran LR, Fossdal JB. Wave induced wind fluctuations relevant to sea skimming missile flight[C]// 35th Aerospace Science Meeting and Exhibition, Reno, 1997:0638-0646.
[12]
苗瑞生, 居贤铭, 吴甲生. 导弹空气动力学[M]. 北京: 国防工业出版社, 2006:346-546.
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