Bat-inspired integrally actuated membrane wings with leading-edge sensing

被引:13
|
作者
Buoso, Stefano [1 ]
Dickinson, Benjamin T. [2 ]
Palacios, Rafael [3 ]
机构
[1] Univ Zurich, Inst Physiol, CH-8057 Zurich, Switzerland
[2] US Air Force, Res Lab, Munit Directorate, Eglin AFB, FL 32542 USA
[3] Imperial Coll London, Dept Aeronaut, London SW7 2AZ, England
基金
英国工程与自然科学研究理事会;
关键词
dielectric elastomers; membrane; feedforward control; gust rejection; AIR VEHICLE WINGS; AEROMECHANICS; FLIGHT;
D O I
10.1088/1748-3190/aa9a7b
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper presents a numerical investigation on the closed-loop performance of a two-dimensional actuated membrane wing with fixed supports. The proposed concept mimics aerodynamic sensing and actuation mechanisms found in bat wings to achieve robust outdoor flight: firstly, variable membrane tension, which is obtained in bats through skeleton articulation, is introduced through a dielectric-elastomer construction; secondly, leading-edge airflow sensing is achieved with bioinspired hair-like sensors. Numerical results from a coupled aero-electromechanical model show that this configuration can allow for the tracking of prescribed lift coefficient signals in the presence of disturbances from atmospheric gusts. In particular, disturbance measurements through the hair sensor (a feedforward control strategy) are seen to provide substantial advantage with respect to a reactive (feedback) control strategy determining a reduction of the oscillations of the lift coefficient.
引用
收藏
页数:11
相关论文
共 50 条
  • [11] Noise reduction mechanism of airfoils with leading-edge serrations and surface ridges inspired by owl wings
    Wang, Lei
    Liu, Xiaomin
    Li, Dian
    PHYSICS OF FLUIDS, 2021, 33 (01)
  • [12] Leading-edge vortex dynamics on plunging airfoils and wings
    Son, O.
    Gao, A-K
    Gursul, I
    Cantwell, C. D.
    Wang, Z.
    Sherwin, S. J.
    JOURNAL OF FLUID MECHANICS, 2022, 940
  • [13] Effect of leading-edge curvature on the aerodynamics of insect wings
    Bhat, Shantanu S.
    Thompson, Mark C.
    INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2022, 93
  • [14] Improving performances of biomimetic wings with leading-edge tubercles
    Giorgio Moscato
    Jais Mohamed
    Giovanni Paolo Romano
    Experiments in Fluids, 2022, 63
  • [15] AERODYNAMICS OF MANEUVERING SLENDER WINGS WITH LEADING-EDGE SEPARATION
    TAVARES, TS
    MCCUNE, JE
    AIAA JOURNAL, 1993, 31 (06) : 977 - 986
  • [16] LEADING-EDGE SEPARATION FROM DELTA-WINGS
    EDWARDS, RH
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (02): : 134 - 135
  • [17] Leading-edge vortex shedding from rotating wings
    Kolomenskiy, Dmitry
    Elimelech, Yossef
    Schneider, Kai
    FLUID DYNAMICS RESEARCH, 2014, 46 (03)
  • [18] LATERAL AERODYNAMICS OF DELTA WINGS WITH LEADING-EDGE SEPARATION
    KATZ, J
    AIAA JOURNAL, 1984, 22 (03) : 323 - 328
  • [19] Improving performances of biomimetic wings with leading-edge tubercles
    Moscato, Giorgio
    Mohamed, Jais
    Romano, Giovanni Paolo
    EXPERIMENTS IN FLUIDS, 2022, 63 (09)
  • [20] LIFT OF DELTA-WINGS WITH LEADING-EDGE BLOWING
    TAVELLA, DA
    JOURNAL OF AIRCRAFT, 1988, 25 (06): : 522 - 524