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昆虫翼拍动中受载变形的粘弹性本构模型

鲍麟 胡劲松 余永亮 程鹏 续伯钦 童秉纲

鲍麟, 胡劲松, 余永亮, 程鹏, 续伯钦, 童秉纲. 昆虫翼拍动中受载变形的粘弹性本构模型[J]. 应用数学和力学, 2006, 27(6): 655-662.
引用本文: 鲍麟, 胡劲松, 余永亮, 程鹏, 续伯钦, 童秉纲. 昆虫翼拍动中受载变形的粘弹性本构模型[J]. 应用数学和力学, 2006, 27(6): 655-662.
BAO Lin, HU Jin-song, YU Yong-liang, CHENG Peng, XU Bo-qing, TONG Bing-gang. Viscoelastic Constitutive Model Related to Deformation of Insect Wing Under Loading in Flapping Motion[J]. Applied Mathematics and Mechanics, 2006, 27(6): 655-662.
Citation: BAO Lin, HU Jin-song, YU Yong-liang, CHENG Peng, XU Bo-qing, TONG Bing-gang. Viscoelastic Constitutive Model Related to Deformation of Insect Wing Under Loading in Flapping Motion[J]. Applied Mathematics and Mechanics, 2006, 27(6): 655-662.

昆虫翼拍动中受载变形的粘弹性本构模型

基金项目: 国家自然科学基金资助项目(903050091023201010072066);中国科学院创新项目(KJCX-SW-L04,KJCX2-SW-L2)
详细信息
    作者简介:

    鲍麟(1979- ),男,江苏徐州人,在读博士生(Tel:+86-10-88256133;E-mail:l.bao@263.net);童秉纲(联系人.Tel:+86-10-88256264;Fax:+86-10-88256133).

  • 中图分类号: O345;Q66

Viscoelastic Constitutive Model Related to Deformation of Insect Wing Under Loading in Flapping Motion

  • 摘要: 昆虫翼拍动受载时发生被动变形,被看作为有助于改善飞行性能的机制之一.决定这种被动变形大小的一个关键因素是昆虫翼的材料本构关系,至今缺乏研究.基于蜻蜓翼(离体)的应力松弛实验和模型翼拍动时受载变形的有限元数值分析,揭示了粘弹性本构关系是昆虫翼材料性能的合理描述,并研究了粘弹性参数对被动变形的影响.
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出版历程
  • 收稿日期:  2005-10-17
  • 修回日期:  2006-02-10
  • 刊出日期:  2006-06-15

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