固体火箭技术Issue(2)：167-171,177,6.DOI:10.7673/j.issn.1006-2793.2014.02.005
基于Kriging方法的整流罩气动外形设计优化
Aerodynamic shape design optimization of fairing based on Kriging method
摘要
Abstract
The aerodynamic shape design optimization of fairing for launch vehicles based on Kriging approximate method was researched.In order to solve the computational complexity problem in aerodynamic shape design optimization of fairing,Kriging func-tion was introduced to establish the approximate model for predicting fairing aerodynamic parameter,the process for parameter esti-mation of Kriging function was deduced,and the specific implementation method was offered.The mathematic model for aerodynamic shape design optimization of fairing was established,and resolved with Kriging method.Simulation results show that convergence effi-ciency of proposed design method is more efficient,the average drag of optimal scheme is 22.2% less than the primary scheme,and all constraint conditions are well satisfied.All research finds can provide theoretical reference for aerodynamic shape design optimiza-tion of flight vehicles.关键词
整流罩/气动外形/设计优化/Kriging函数Key words
fairing/aerodynamic shape/design optimization/Kriging function分类
航空航天引用本文复制引用
杨希祥,周张,彭科..基于Kriging方法的整流罩气动外形设计优化[J].固体火箭技术,2014,(2):167-171,177,6.基金项目
国防科技大学科研计划资助项目（ JC12-01-05）。 （）
