摘要
基于Kriging代理模型,建立了一种考虑膜片半径与厚度、锥段高度与角度等典型结构特征的计算屈曲载荷的工程方法,并选取典型样本点对模型进行了数值验证.结果表明:基于Cubic相关函数建立的Kriging代理模型预测未知样本点屈曲载荷误差控制在5%以内,较常用的Gauss相关函数更适合建立锥柱形膜片屈曲载荷的Kriging代理模型;此代理模型能准确计算未知样本点的屈曲载荷,减少了繁杂的有限元建模与计算过程;根据设定的屈曲载荷,代理模型可计算各典型特征的参数值,并可作为锥柱形膜片结构优化设计的约束函数或目标函数.
Regarding typical structural characteristics of radius and thickness of diaphragms, height and angle of cone section, a method was built to compute the buckling load of diaphragms based on Kriging metamodel. The Kriging metamodel was validated by typical samples. Research results show that: for the Kriging metamodel based on Cubic correlation function, the error percentage to compute buckling loads at untried inputs is less than 5 %, more suitable for computing the buckling loads of spherical-cone diaphragms than that based on Gauss correlation function; the metamodel could precisely compute buckling loads at untried inputs, without need of modeling and simulation by finite element method; the metamodel could compute parameter values of typical structural characteristics according to a set buckling load, and also could be used as bound function or object function for structural optimization design of spherical-cone diaphragms.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2014年第1期111-117,共7页
Journal of Aerospace Power
基金
国家重点基础研究发展计划(61338)