Journal Home Online First Current Issue Archive For Authors Journal Information 中文版

Strategic Study of CAE >> 2009, Volume 11, Issue 5

The development of aerodynamics & configurationtechnology for large aircraft

China Aviation Industry Corporation, Beijing 100712,China

Received: 2008-11-17 Available online: 2009-05-13 14:59:41.000

Next Previous

Abstract

The paper introduced the development of aerodynamics & configuration technology for large aircraft.The technique of fuselage and the advanced aerodynamics configuration — blended wing body (BWB) were described. The impact of aerodynamics & configuration technology on safety, economical, comfortable and environmental characters for large aircraft was analyzed.The proposal for enhancing the research of aerodynamics in China was presented.

Figures

图1

图2

图3

图4

图5

图6

图7

图8

图9

图10

图11

图12

图13

图14

图15

图16

图17

图18

图19

图20

图21

图22

图23

图24

图25

图26

图27

References

[ 1 ] International Monetary Fund.Statistical report of 1997 [ R] .Wash- ington D C,1997

[ 2 ] 刘大响.大型民用飞机发动机的发展现状及关键技术[R].深圳:中国航空学会,2007

[ 3 ] 张彦仲,金德琨.航空电子的新进展[R].北京:中国科学院,2007

[ 4 ] 顾颂芬.新一代大型客机的要求和特点[R].在大飞机方案论证委员会,2006

[ 5 ] 张雨,孙刚,张淼,等.民用飞机翼梢小翼的多约束优化设计[J].空气动力学报,2006,24(3):367-370 link1

[ 6 ] Leibeck R H.Design of the blended wing body subsonic transport [ J] .Journal of Aircraft, 2004 , 41 ( 1 ) :10 -25 link1

[ 7 ] 张彦仲.航空技术的发展趋势[J].中国工程科学,1999,1(1):10 link1

[ 8 ] Charles Champion.Development of Airbus A380.ICAS 2006 , 2006.9

Related Research