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喷气客机总体参数优化计算环境的开发
引用本文:俞金海,周琳,李晨,余雄庆,张帅,王宇.喷气客机总体参数优化计算环境的开发[J].航空工程进展,2011,2(2):163-168.
作者姓名:俞金海  周琳  李晨  余雄庆  张帅  王宇
作者单位:1. 中国商用飞机有限责任公司上海飞机设计研究院,上海,200232
2. 南京航空航天大学航空宇航学院,南京,210016
摘    要:为了满足喷气客机多方面的设计要求和目标,开发了总体参数优化计算环境.基于工程算法,研究了几何、动力、重量、气动、性能、操稳和成本的分析模型,并开发了相应的计算模块;通过集成各专业分析模块,建立了喷气客机总体综合分析模型;在探讨了喷气客机总体参数优化模型的基础上,应用iSIGHT平台集成喷气客机总体综合分析模型,建立了喷...

关 键 词:喷气客机  飞机设计  总体参数优化  计算环境

A Framework for Optimization of Civil Jet Conceptual Design
Yu Jinhai,Zhou Lin,Li Chen,Yu Xiongqing,Zhang Shuai,Wang Yu.A Framework for Optimization of Civil Jet Conceptual Design[J].Advances in Aeronautical Science and Engineering,2011,2(2):163-168.
Authors:Yu Jinhai  Zhou Lin  Li Chen  Yu Xiongqing  Zhang Shuai  Wang Yu
Institution:Yu Jinhai1,Zhou Lin1,Li Chen1,Yu Xiongqing2,Zhang Shuai2,Wang Yu2(1.Shanghai Aircraft Design and Research Institute,Commercial Aircraft Corporation of China,Ltd.,Shanghai 200232,China)(2.College of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)
Abstract:In order to meet the design requirement and aim of civil jet,a computing framework optimization of civil jet conceptual design is developed.Based on the empirical methods of the individual disciplines including geometry,propulsion,mass,aerodynamics,performance,control and cost,the computer codes for each discipline are developed.The global analysis code for civil jet conceptual design is obtained by integration of the codes for each discipline,and an integral conceptual design analytical model is presented....
Keywords:civil jet  aircraft design  conceptual optimization  computing framework  
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