浅析民用飞机研制总体参数优化  

Overall Parameter Optimization for Civil Aircraft Development

作　　者：吴玲琳 李海涛[1] WU Linglin;LI Haitao(Shanghai Aircraft Design and Research Institute,Shanghai 201210,China)

机构地区：[1]上海飞机设计研究院,上海201210

出　　处：《民用飞机设计与研究》2018年第4期79-84,共6页Civil Aircraft Design & Research

摘　　要：分析了在概念设计阶段民用飞机总体设计工作内容和工作流程,并结合时下国外在用软件优缺点,构思了民用飞机总体设计参数综合优化的技术方案,包括优化设计架构、分析模型和优化算法等,为形成具有自主知识产权的民机总体设计综合分析和优化程序打下基础。This article analyzes work content and work process of general design for civil aircraft during concept design phase.Combined with merits and drawbacks of foreign software used presently,we presented technical plan of general design parameters comprehensive optimization,including optimizing design architecture,analyzing model and optimizing arithmetic,which would be a foundation for forming civil aircraft general design combination analysis and optimization program with proprietary intellectual property rights.

关 键 词：民机总体设计 参数优化 分析模型 

分 类 号：V221.6[航空宇航科学与技术—飞行器设计]