飞机结构气—弹耦合非线性颤振的控制
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.
出处
《晋中学院学报》
2012年第3期25-29,共5页
Journal of Jinzhong University
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