摘要
多学科设计优化(MDO)方法是提高飞机设计效率,得到最优设计方案的有效手段。在飞机设计过程中,需要确保飞机静安定裕度满足使用要求,因此需要充分考虑总体、气动等学科专业的耦合效应。针对这一问题,基于MDO软件Modelcenter构建飞机外形多学科优化协同设计流程,通过对某型飞机外形优化设计的实例分析,得到该机的最优外形修改方案,证明了MDO方法在飞机设计中应用的高效性。
Multidisciplinary design optimization(MDO)methods are the effective means to improve the aircraft design efficiency and achieve the optimal design scheme.During the process of aircraft design,the pitching static margin of aircraft must meet the usage requirement,therefore the coupling affections between general layout and aerodynamics must be considered.To solve this problem,apracticable solution is proposed.The collaborative MDO process of aircraft configuration is created based on Modelcenter.The MDO of a certain aircraft configuration is taken as an example.The optimal configuration scheme of this aircraft is obtained.The high effective of MDO methods applied in aircraft design is proved.
作者
邹宁
冯文梁
滕杰
周伟
Zou Ning Feng Wenliang Teng Jie Zhou Wei(Technical Center, Chengdu Aircraft Industrial(Group) Co., Ltd., Chengdu 610092, China)
出处
《航空工程进展》
CSCD
2017年第1期92-97,共6页
Advances in Aeronautical Science and Engineering
关键词
多学科设计优化
飞机设计
静安定裕度
优化算法
外形参数化
multidisciplinary design optimization(MDO)
aircraft design
pitching static margin
optimization algorithm
geometric parameterization