中国机械工程2012，Vol.23Issue(6)：717-720,4.
超弹性蒙皮蜂窝芯的设计及等效模量研究
Design on Flexible Honeycomb and Research on Its Equivalent Modulus
摘要
Abstract
The skin of a morphing wing would be highly anisotropic with low in-plane stiffness and high out-of-plane flexural bending stiffness,having the ability to undergo large strains.The approach of mechanics of material was presented to evaluate the elastic modulus of properties of the U-shape honeycomb.The U-shape honeycomb was proved to have low in-plane axial stiffness,which has a good flexibility and low modulus in certain direction and high load resistance.Both of finite-element modeling and experimental testing were carried out to verify the accuracy of the proposed analytical formulation.The analytical solutions developed compared well with both experimental test and FE modeling.The FE modeling of a large area was also carried out to get the Possion＇s ratio of the honeycomb.The simplified analyses and formulation presented for U-shape cores can be used in design and optimization of efficient cellular core structures.关键词
智能变形飞行器/超弹性蒙皮结构/蜂窝芯结构/等效弹性模量Key words
morphing aircraft/superelastic skin structure/honeycomb core/equivalent modulus分类
通用工业技术引用本文复制引用
彭海峰,董二宝,张世武,杨杰..超弹性蒙皮蜂窝芯的设计及等效模量研究[J].中国机械工程,2012,23(6):717-720,4.基金项目
国家自然科学基金资助项目 （）
中国博士后科学基金资助项目 （）
