[1]薛澄岐,尤志芳.基于航空飞行器冰雹撞击试验的冰雹粒子特性分析[J].东南大学学报(自然科学版),2009,39(6):1165-1168.[doi:10.3969/j.issn.1001-0505.2009.06.016]
 Xue Chengqi,You Zhifang.Hail particles characteristic analysis based on aviation aircraft hail impact test[J].Journal of Southeast University (Natural Science Edition),2009,39(6):1165-1168.[doi:10.3969/j.issn.1001-0505.2009.06.016]
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基于航空飞行器冰雹撞击试验的冰雹粒子特性分析()
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《东南大学学报(自然科学版)》[ISSN:1001-0505/CN:32-1178/N]

卷:
39
期数:
2009年第6期
页码:
1165-1168
栏目:
数学、物理学、力学
出版日期:
2009-11-20

文章信息/Info

Title:
Hail particles characteristic analysis based on aviation aircraft hail impact test
作者:
薛澄岐 尤志芳
东南大学机械工程学院, 南京 210096
Author(s):
Xue Chengqi You Zhifang
School of Mechanical Engineering, Southeast University, Nanjing 210096, China
关键词:
冰雹 飞行器 撞击 冲击波
Keywords:
hail aircraft impact stock wave
分类号:
O347.3
DOI:
10.3969/j.issn.1001-0505.2009.06.016
摘要:
为了研究冰雹高速撞击对航空飞行器造成的损伤,需构建相应的试验系统,其中冰雹粒子特性分析是关键.从航空飞行器冰雹撞击试验的要求出发,对冰雹粒子的特性进行了全面分析.首先应用冲击波理论分析了冰雹破坏特性,以及冰雹出现裂纹的条件; 然后对冰雹撞击运动过程进行了建模,给出了基于简单波的冰雹粒子运动方程; 最后给出了冰雹撞击试验系统参数的计算程序.据此确定了冰雹撞击试验系统设计参数:撞击速度200~300 m/s,冰雹直径19 mm,气压0.6~1.0 MPa,气体炮炮管长度6 m.在此基础上成功开发国内首台冰雹试验系统,该系统所有特性均达到设计标准,证明了理论分析是正确的,符合冰雹撞击试验实际情况和要求.
Abstract:
In order to study the hail impact damage on aerospace vehicles, it is very necessary to construct the corresponding experimental system, and characteristic analysis of ice particles is the key. From the aviation aircraft hail impact test requirements, the characteristics of hail particles are fully analyzed in this paper. Firstly, hail damage characteristics and hail cracks condition are analyzed by shock wave theory. Secondly, hail impact movement is modeled and hail particle movement equations based on simple wave are built. Finally, calculation program is scheduled to obtain the parameters of hail impact test system. Accordingly the hail impact test system design parameters are determined, i.e., impact velocity 200-300 m/s, hail diameter 19 mm, pneumatic 0.6-1.0 MPa, air cannon tube length 6 m. On this basis, first domestic hail test system is developed successfully. All properties of system achieve the design standards. It proves the correctness of theoretical analysis which is in accord with the actual situation and requirements of the hail impact test.

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备注/Memo

备注/Memo:
作者简介: 薛澄岐(1961—),男,博士,教授,ipd_xcq@seu.edu.cn.
基金项目: 航空科学基金资助项目(20085569014).
引文格式: 薛澄岐,尤志芳.基于航空飞行器冰雹撞击试验的冰雹粒子特性分析[J].东南大学学报:自然科学版,2009,39(6):1165-1168. [doi:10.3969/j.issn.1001-0505.2009.06.016]
更新日期/Last Update: 2009-11-20