The low - velocity impact response of composite laminated structures is very important.
冲击器与复合材料接触性态的研究是复合材料低速冲击响应研究的关键.
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The low - velocity impact response of Nomex honeycomb sandwich plate was investigated theoretically and experimentally.
给出了基于Mindlin板理论并考虑到夹芯板上下纤维增强层板在撞击时变形不同的用于撞击动响应计算的分析模型.
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