Aerodynamics of the Wing/Fuselage Junction at an Transport Aircraft in High-Lift Configuration

被引：0

作者：

Melber-Wilkending, Stefan ^{[1
]}

机构：

[1] German Aerosp Ctr DLR, Inst Aerodynam & Flow Technol, D-38108 Braunschweig, Germany

来源：

NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS VII | 2010年 / 112卷

关键词：

D O I：

10.1007/978-3-642-14243-7_65

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

This paper presents the numerical simulation (DLR TAU-code) and the analysis of viscous high-lift flow around a complex wing/body configuration (DLR ALVAST) in landing configuration. The investigations aim for a better understanding of the aerodynamics at the wing root and the lift breakdown for such a configuration.

引用

页码：529 / 536

页数：8

共 10 条

[1]

FLAIG A, 1993, AGARDCP515

[2]

KALLINDERIS Y, 1999, HDB GRID GENERATION

[3]

KROLL N, 2002, 23 ICAS C ICAS 2002

[4]

Melber S, 2002, NOTE NUM FL, V77, P27

[5]

MELBERWILKENDIN.S, 2004, 14 AG STAB DGLR S NO

[6]

MELBERWILKENDIN.S, 2006, 15 AG STAB DGLR S DA

[7]

PUFFERTMEISSNER W, 1996, 1B1299620 DLR

[8] Aerodynamic design of the high-lift-wing for a Megaliner aircraft [J].

Reckzeh, D .

AEROSPACE SCIENCE AND TECHNOLOGY, 2003, 7 (02) :107-119

[9]

RUDNIK R, 2000, 20004326 AIAA

[10]

SCHWETZLER D, 1995, HIGH LIFT SEP CONTR

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