几何非线性在机翼结构设计中的影响研究

基于MARC2003非线性有限元计算软件,比较翼根短盒段、翼根长盒段以及整体机翼结构的非线性稳定性分析结果。通过上述比较发现工程上常用的方法,即以危险部位代替整体结构并以线性计算出的节点位移,作为非线性计算的边界条件进行非线性稳定性计算,将会带来较大的误差,因此不宜在稳定性设计中采用。随后,从机翼挠度变形和翼尖扭角两个方面出发,通过与线性分析相比较,阐明非线性行为随飞行过载演变的历程,从而得出结论,在过载系数小于2时非线性对挠度变形的影响不大,相比之下非线性对扭角的影响却尤为突出,因此在机翼扭转刚度设计以及气动弹性设计中必须考虑非线性的影响。

RESEARCH ON THE INFLUENCE OF GEOMETRIC NONLINEARITY IN THE WING STRURE DESIGN

Based on MARC2003 nonlinear finite element calculation software,the thesis compared the results of nonlinear stability analysis of the short box,the long box and the whole wing structure.The result indicates that using important part in place of the whole structure and using the node displacements calculated by linear calculation as a boundary conditions for nonlinear analysis are not proper.This technique should not be used in the stability design.By the deflection and the torsion angle,compared with linea...