基于响应面法的机翼气动-结构多学科优化设计  

Aerodynamic-structure Multidisciplinary Optimization Design of Wing Based on Response Surface Methodology

作　　者：刘金辉[1] 乔志德[1] 杨旭东[1] 郝国芬[2] 

机构地区：[1]西北工业大学翼型叶栅空气动力学国防科技重点实验室 [2]河北工程技术高等专科学校计算中心,河北沧州061036

出　　处：《空军工程大学学报（自然科学版）》2006年第1期1-3,共3页Journal of Air Force Engineering University(Natural Science Edition)

基　　金：国家自然科学基金资助项目(10402036)

摘　　要：应用响应面法进行了弹性机翼的气动-结构多学科优化设计方法研究。以M6机翼为初始机翼,进行了多目标、多约束的气动-结构优化设计,优化后的机翼具有较好的气动-结构综合性能,升阻比增加了9.25%,而重量减轻了4.84%;模型精度满足设计要求。优化结果表明所发展的优化设计方法是成功有效的,具有重要的应用价值。In this paper, the multidisciplinary aerodynamic - structure optimization design method of elastic wing based on response surface methodology is performed. M6 wing is chosen as the base wing. The design results show that the lift - to - drag ratio has increased by 9.25% and the structural weight has reduced by 4.84% , the response surface methodology is accurate enough to satisfy the engineering requirement. It can be concluded that the present method is effective and feasible, and is applicable for engineering practice due to its high design capability.

关 键 词：响应面法 欧拉方程 有限元方法 静气动弹性 

分 类 号：V224[航空宇航科学与技术—飞行器设计]