Numerical and experimental transition results evaluation for a morphing wing and aileron system

被引：30

作者：

Botez, R. M. ^{[1
]}

Koreanschi, A. ^{[1
]}

Gabor, O. S. ^{[1
]}

Tondji, Y. ^{[1
]}

Guezguez, M. ^{[1
]}

Kammegne, J. T. ^{[1
]}

Grigorie, L. T. ^{[1
]}

Sandu, D. ^{[1
]}

Mebarki, Y. ^{[2
]}

Mamou, M. ^{[2
]}

Amoroso, F. ^{[3
]}

Pecora, R. ^{[3
]}

Lecce, L. ^{[3
]}

Amendola, G. ^{[4
]}

Dimino, I. ^{[4
]}

Concilio, A. ^{[4
]}

机构：

[1] Ecole Technol Super, Res Lab Act Control, Avion & AeroServoElast LARCASE, Montreal, PQ, Canada

[2] NRC Aerosp, Aerodynam Lab, Ottawa, ON, Canada

[3] Univ Naples Federico II, Ind Engn Dept, Aerosp Div, Naples, Italy

[4] Italian Aerosp Res Ctr CIRA, Adapt Struct Div, Capua, CE, Italy

来源：

AERONAUTICAL JOURNAL | 2018年 / 122卷 / 1251期

基金：

加拿大自然科学与工程研究理事会;

关键词：

aerodynamics; Morphing Wing Tip; Genetic Optimization Algorithm; Flow Transition; Drag Coefficient Reduction; Wind Tunnel Tests; Morphing Aileron Classification Description: Aerodynamics; Aeroelasticity; Avionics and Systems; Computational Fluid Dynamics; Experimental Fluid Dynamics; LOW-SPEED; OPTIMIZATION; DESIGN;

D O I：

10.1017/aer.2018.15

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

A new wing-tip concept with morphing upper surface and interchangeable conventional and morphing ailerons was designed, manufactured, bench and wind-tunnel tested. The development of this wing-tip model was performed in the frame of an international CRIAQ project, and the purpose was to demonstrate the wing upper surface and aileron morphing capabilities in improving the wing-tip aerodynamic performances. During numerical optimisation with 'in-house' genetic algorithm software, and during wind-tunnel experimental tests, it was demonstrated that the air-flow laminarity over the wing skin was promoted, and the laminar flow was extended with up to 9% of the chord. Drag coefficient reduction of up to 9% was obtained when the morphing aileron was introduced.

引用

页码：747 / 784

页数：38

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