| 史明丽,黄国强.冲击基本设计试验条件对机载外挂的适用性分析[J].装备环境工程,2012,9(2):17-20. SHI Ming-li,HUANG Guo-qiang.Applicability Analysis of Basic Shock Test Condition on Aerocraft External Carry[J].Equipment Environmental Engineering,2012,9(2):17-20. |
| 冲击基本设计试验条件对机载外挂的适用性分析 |
| Applicability Analysis of Basic Shock Test Condition on Aerocraft External Carry |
| 投稿时间：2011-11-14 |
| DOI： |
| 中文关键词: 冲击 着陆环境 半正弦波 后峰锯齿波 冲击响应谱 |
| 英文关键词:shock landing shock half-sine pulse terminal peak sawtooth pulse SRS |
| 基金项目:中文基金项目 |
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| 中文摘要: |
| 借助冲击响应谱理论，分析了GJB150.18系列标准中规定的飞行器设备冲击基本设计试验条件和机载外挂物着陆冲击试验条件的等效关系，理清了冲击基本设计试验条件考核机载外挂物的适用性问题，提出了机载外挂物挂机飞行、着陆过程中冲击环境的考核方法。 |
| 英文摘要: |
| The equivalent relation between basic design test condition and landing shock test condition of aerocraft external carry stated in GJB 150.18was analyzed using shock response spectrum theory. The applicability of using basic design test condition for aerocraft external carry was studied. The shock test methods for aerocraft external carry in flight and landing process were put forward. |
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