| 翼身融合飞机的空气动力学研究进展 |
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| 引用本文： | 李晓勇,张淼,鲁素芬,李栋成,周涛.翼身融合飞机的空气动力学研究进展[J].飞机设计,2007,27(2):1-9,20. |
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| 作者姓名： | 李晓勇 张淼 鲁素芬 李栋成 周涛 |
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| 作者单位： | 中航第一飞机研究院,总体气动室,上海,200232 |
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| 摘 要： | 翼身融合飞机(Blended Wing Body Aircraft-BWB Aircraft)是一种新型高升阻比无尾布局的大型运输机,其气动特性的研究是BWB布局飞机克服众多技术难题的基础。文章首先简述了BWB布局的研究历程,给出巨型BWB布局飞机的总体几何特征参数和基本性能,并简述风洞和自由飞试验情况;接着介绍BWB研究中的多学科优化平台,着重讨论气动优化技术,它是解决BWB布局气动问题的基础手段之一;然后综述BWB布局研究的热点领域:气动特性研究、气动弹性研究和发动机/机体一体化设计研究;最后提出BWB布局发展趋势的若干方面。
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| 关 键 词： | BWB布局 气动特性 优化设计 |
| 文章编号： | 1673-4599（2007）02-0001-09 |
| 收稿时间： | 2006-08-07 |
| 修稿时间： | 2006-08-072007-03-15 |
Advances in Aerodynamics for Blended-Wing-Body Aircraft |
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| LI Xiao-yong,ZHANG Miao,LU Su-fen,LI Dong-cheng,ZHOU Tao.Advances in Aerodynamics for Blended-Wing-Body Aircraft[J].Aircraft Design,2007,27(2):1-9,20. |
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| Authors: | LI Xiao-yong ZHANG Miao LU Su-fen LI Dong-cheng ZHOU Tao |
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| Institution: | Department 1, The First Aircraft Institute of AVIC-1, Shanghai 200232, China |
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| Abstract: | Blended-Wing-Body(BWB)aircraft is a tailless large transport with high lift-drag ratio,and the aerodynamic study for BWB aircraft is a basis of overcoming the technology challenges about it.Firstly,research history on BWB configuration is presented in this paper;geometric parameters and basic performances of BWB configuration are discussed;and wind tunnel experiments and free flight tests for large BWB aircraft are described.Secondly,multidisciplinary optimization design technologies applied to the BWB aircraft,especially aerodynamic optimization design technologies,which are one of basic ways for solving BWB aerodynamic problems,are discussed.Thirdly,major issues of BWB configuration research,such as aerodynamic characteristics,aeroelastic design and integrated engine/body design,are given.Finally,some further works about BWB configuration study are proposed. |
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| Keywords: | BWB configuration aerodynamic characteristics optimization design |
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