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    Measurement of a Bluff Body Aerodynamic Yaw Moment Magnification and Damping Using a Dynamic Wind Tunnel Facility 

    Source: Journal of Applied Mechanics:;2011:;volume( 078 ):;issue: 003:;page 31004
    Author(s): Shuhaimi Mansor; Martin Passmore
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a technique for determining the dynamic aerodynamic yaw moment derivative based on the time response data using an oscillating model rig. The aerodynamic yaw moment derivatives ...
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    Design Parametric Study of a Compound Wing-in-Ground Effect. II: Aerodynamics Coefficients 

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 001
    Author(s): Saeed Jamei; Adi Maimun; Shuhaimi Mansor; Nor Azwadi; Agoes Priyanto
    Publisher: American Society of Civil Engineers
    Abstract: The aerodynamic behavior of the wing-in-ground effect can be affected by its configuration. This configuration is potentially the most influential parameter for the performance and stability of the wing-in-ground effect ...
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    Design Parametric Study of a Compound Wing-in-Ground Effect. I: Aerodynamics Performance 

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 001
    Author(s): Saeed Jamei; Adi Maimun; Shuhaimi Mansor; Nor Azwadi; Agoes Priyanto
    Publisher: American Society of Civil Engineers
    Abstract: The configuration and service condition of a wing can influence the performance of wing-in-ground effect (WIG) craft. In this study, the aerodynamic performance of compound wings in ground effect was numerically investigated ...
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    Design Parametric Study of a Compound Wing-in-Ground Effect. II: Aerodynamics Coefficients 

    Source: Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 001
    Author(s): Saeed Jamei; Adi Maimun; Shuhaimi Mansor; Nor Azwadi; Agoes Priyanto
    Publisher: American Society of Civil Engineers
    Abstract: The aerodynamic behavior of the wing-in-ground effect can be affected by its configuration. This configuration is potentially the most influential parameter for the performance and stability of the wing-in-ground effect ...
    Request PDF
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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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