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    Dynamic Fluid-Structure Coupling Method of Flexible Flapping Wing for MAV 

    Source: Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 006
    Author(s): Wenqing Yang; Bifeng Song; Liguang Wang; Lili Chen
    Publisher: American Society of Civil Engineers
    Abstract: This paper presents a numerical method to simulate the dynamic interaction between the structural deformation and the aerodynamic characteristics of flexible flapping wing for micro air vehicle (MAV). A fluid-structure ...
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    Influence of Different Take-Off Weights on the Longitudinal Dynamic Stability of Flapping-Wing MAVs 

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 003:;page 04021006-1
    Author(s): Dong Xue; Bifeng Song; Wenping Song; Wenqing Yang; Wenfu Xu
    Publisher: ASCE
    Abstract: Due to different requirements of flight tasks, take-off weights vary according to different payloads, which will definitely influence the trim characteristics and flight dynamics of vehicles. When the mass ratio between ...
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    The Effect of Unsteady Flapping Motion on the Aerodynamic Performance of Bio-Inspired Alula 

    Source: Journal of Aerospace Engineering:;2022:;Volume ( 035 ):;issue: 003:;page 04022018
    Author(s): Han Bao; Dongfu Ma; Wenqing Yang; Bifeng Song; Dong Xue
    Publisher: ASCE
    Abstract: Avian flight has inspired scientists and engineers for a long time. Flapping-wing micro air vehicle (FMAV) is a kind of air vehicle mimicking the avian flapping flight that has achieved great success in this century. ...
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    DSpace software copyright © 2002-2015  DuraSpace
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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