提出了敷设粘弹性阻尼层的复合材料层合结构随机振动分析的高效精确算法.考虑了粘弹性阻尼材料对激振频率的依赖性及Adams提出的复合材料层合结构的阻尼模型.为解决依赖频率变化的非经典阻尼的复杂结构,结合实模态降阶直接解法对虚拟激励法做了相应的发展,精确求解了降阶后的随机振动方程.以国产有限元程序系统DDJ为平台开发了相应的程序,并对波音737客机的水平尾翼的复合材料安定面结构进行模拟研究,从复杂的计算及合理的结论可以看出,本文中所提出的方法对复合材料的随机振动分析十分有效.
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