空气动力学学报2017，Vol.35Issue(4)：516-528,13.DOI:10.7638/kqdlxxb-2017.0058
飞行器气动外形设计方法研究与进展
Aerodynamic shape design methods for aircraft: status and trends
摘要
Abstract
The continuous development of computer technology and computational fluid dynamics has led to great progress in aerodynamic shape design methods. Aerodynamic design methods have been developed from cut-and-try to reverse design and further to optimal design. Aerodynamic analysis methods have been evolved from wind tunnel test to low fidelity computational fluid dynamics (CFD) and then to high fidelity CFD simulation. With the higher and higher requirements regarding aircraft performance, the design conditions, optimization models and design constraints are becoming more and more complex. Consequently, the continuously increasing number of design variables and design goals lead to new challenges for aerodynamic design methods. Based on years of research experiences by the author and author''s team and the domestic and abroad related research findings, aerodynamic shape design methods are systematically reviewed in the present paper. New problems and challenges in aerodynamic design are summarized. Moreover, future research trends of aerodynamic shape design are prospected.关键词
气动外形设计/反设计/优化设计/多目标优化/稳健性设计Key words
aerodynamic shape design/inverse design/optimal design/multi-objective design/robust design分类
航空航天引用本文复制引用
高正红,王超..飞行器气动外形设计方法研究与进展[J].空气动力学学报,2017,35(4):516-528,13.基金项目
国家自然科学基金(11372254) （11372254）
