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[an error occurred while processing this directive]Compilation of Vibration Test Conditions Based on Mechanical Measure for a Missile
Received date: 2016-02-29
Online published: 2025-05-30
翟唤春 , 赵鑫 , 孔小林 , 李博 . 基于力学环境实测的某型导弹振动试验条件制定[J]. 弹箭与制导学报, 2016 , 36(4) : 137 -140,145 . DOI: 10.15892/j.cnki.djzdxb.2016.04.036
To improve credibility of reliability qualification test, environmental conditions of launching and flight process for a missile must be reproduced accurately. Based on actually measured data obtained from launching and flight process of a missile, the analysis on data was made, and the inductive method was given for the actually measured spectrum and normative spectrum of vibration. The vibration test condition forms which can be used in reliability qualification test. The practice has proved that the method meets requirements of engineering application and the operational procedure is chosen rightly and can be easily realized.
Key words: missile; actual measure; vibration test
| [1] | 施荣明, 朱广荣, 吴飒,等. 军用装备实验室环境试验方法第16部分:振动试验:GJB150A-2009[S]. 北京:中国标准出版社, 2009: 5, 14. |
| [2] | 徐明, 孙建勇, 李宪珊,等. 振动、冲击环境测量数据归纳方法:GJB/Z126—99[S]. 北京:中国标准出版社, 1999: 2- 5. |
| [3] | 袁宏杰, 罗敏, 姜同敏. 随机振动环境测量数据归纳方法研究. 航空学报, 2007, 28 (1): 115- 117. |
| [4] | 张阿舟, 张克荣. 振动环境工程[M]. 北京:航空工业出版社, 1986: 374- 379. |
| [5] | 刘凯. 基于实测数据的空空导弹自由飞振动条件制定方法研究 装备环境工程, 2014, 11 (5): 114- 118. |
| [6] | 董欣, 俞云书, 夏益霖,等. 动力学环境数据采集和分析指南:GJB/Z222-2005[S]. 北京:中国标准出版社, 2005: 2- 57. |
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