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
收藏
页码：747 / 784
页数：38
相关论文
共 50 条
  • [1] Numerical and experimental validation of a full scale servo-actuated morphing aileron model
    Arena, Maurizio
    Amoroso, Francesco
    Pecora, Rosario
    Amendola, Gianluca
    Dimino, Ignazio
    Concilio, Antonio
    SMART MATERIALS AND STRUCTURES, 2018, 27 (10)
  • [2] Employing Wing Morphing to Cooperate Aileron Deflection Improves the Rolling Agility of Drones
    Liu, Yubin
    Zhang, Junming
    Gao, Liang
    Zhu, Yanhe
    Liu, Benshan
    Zang, Xizhe
    Cai, Hegao
    Zhao, Jie
    ADVANCED INTELLIGENT SYSTEMS, 2023, 5 (11)
  • [3] Experimental Validation and Evaluation of a Coupled Twist-Camber Morphing Wing Concept
    do Vale, Jose Lobo
    Raffaelli, John
    Suleman, Afzal
    APPLIED SCIENCES-BASEL, 2021, 11 (22):
  • [4] Effects of an Unsteady Morphing Wing with Seamless Side-Edge Transition on Aerodynamic Performance
    Abdessemed, Chawki
    Bouferrouk, Abdessalem
    Yao, Yufeng
    ENERGIES, 2022, 15 (03)
  • [5] Smart materials applied in a micro remotely piloted aircraft system with morphing wing
    Barcala-Montejano, Miguel A.
    Rodriguez-Sevillano, Angel A.
    Bardera-Mora, Rafael
    Garcia-Ramirez, Jaime
    de Nova-Trigueros, Joaquin
    Urcelay-Oca, Inigo
    Morillas-Castellano, Israel
    JOURNAL OF INTELLIGENT MATERIAL SYSTEMS AND STRUCTURES, 2018, 29 (16) : 3317 - 3332
  • [6] Design and wind tunnel experimental validation of a controlled new rotary actuation system for a morphing wing application
    Kammegne, Michel Joel Tchatchueng
    Grigorie, Lucian Teodor
    Botez, Ruxandra Mihaela
    Koreanschi, Andreea
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 230 (01) : 132 - 145
  • [7] Simple adaptive wing-aileron flutter suppression system
    Vindigni, Carmelo Rosario
    Mantegna, Giuseppe
    Orlando, Calogero
    Alaimo, Andrea
    JOURNAL OF SOUND AND VIBRATION, 2024, 570
  • [8] A combined experimental-numerical analysis of a novel deformable sandwich structure for morphing wing applications
    Hajarian, Amin
    Zakerzadeh, Mohammad Reza
    Salehi, Hamid
    Baghani, Mostafa
    JOURNAL OF SANDWICH STRUCTURES & MATERIALS, 2021, 23 (08) : 4054 - 4076
  • [9] Evaluation of a Compliant Droop-Nose Morphing Wing Tip via Experimental Tests
    Vasista, Srinivas
    Riemenschneider, Johannes
    van de Kamp, Bram
    Monner, Hans Peter
    Cheung, Ronald C. M.
    Wales, Christopher
    Cooper, Jonathan E.
    JOURNAL OF AIRCRAFT, 2017, 54 (02): : 519 - 534
  • [10] Fuzzy Logic-Based Control for a Morphing Wing Tip Actuation System: Design, Numerical Simulation, and Wind Tunnel Experimental Testing
    Khan, Shehryar
    Grigorie, Teodor Lucian
    Botez, Ruxandra Mihaela
    Mamou, Mahmoud
    Mebarki, Youssef
    BIOMIMETICS, 2019, 4 (04)
12345