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飞机结构气—弹耦合非线性颤振的控制

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摘要 非线性气动弹性理论研究为先进飞机结构设计提供了理论指导,也为消除和预防不希望发生的气弹不稳定振动奠定必要的基础.智能材料的应用应是先进飞机颤振抑制技术走向实用化的有效途径.由于形状记忆合金具有高阻尼、大回复力、大应变容量及其抗疲劳性能强等方面的优势,在今后的颤振抑制应用研究中必将发挥更大作用.
作者 张晓梅 任勇生
机构地区 山西煤炭职业技术学院计算机信息系 山东科技大学机械电子工程学院
出处 《晋中学院学报》 2012年第3期25-29,共5页 Journal of Jinzhong University
关键词 非线性 气弹性动力学 壁板与壳体 极限环震荡 颤振抑制
分类号 TB53 [理学—声学]
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参考文献37

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二级参考文献18

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共引文献4

晋中学院学报
2012年 第3期

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