High-lift aerodynamics design for large civil aircraft in Fudan university

被引：0

作者：

Sun Gang ^{[1
]}

Xu Kangle ^{[1
]}

Chen Yingchun ^{[2
]}

机构：

[1] Fudan Univ, Mech & Engn Sci Dep, Shanghai 200433, Peoples R China

[2] Shanghai Aircraft Design & Res Inst, COMAC, Shanghai 200235, Peoples R China

来源：

ADVANCES IN MECHANICAL ENGINEERING, PTS 1-3 | 2011年 / 52-54卷

关键词：

high-lift system; aerodynamics design; large civil aircraft;

D O I：

10.4028/www.scientific.net/AMM.52-54.1382

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

Part of work on CFD simulations by the high-lift system design team in Fudan university for large civil aircraft is presented. The research on CFD simulation of the high-lift systems and some concepts and experience in three-dimensional geometry modeling are also presented, which are done on the self-developed platform of high-lift device aerodynamic calculation software and programs. For which, the design efficiency is substantially improved.

引用

页码：1382 / +

页数：2

共 6 条

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[2] Advanced technology and development of high lift system for civil aircraft
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[3] Design of automatic climbing controller for large civil aircraft
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[4] Aerodynamic design of the high-lift-wing for a Megaliner aircraft
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[5] Progress of adjoint-based aerodynamic optimization design for large civil aircraft
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[6] Aerodynamic optimization design of large civil aircraft wings using surrogate-based model
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