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    Aerodynamic Analysis of Flexible Flapping Wing Micro Aerial Vehicle Using Quasi-Steady Approach

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    Aerodynamic Analysis of Flexible Flapping Wing Micro Aerial Vehicle Using Quasi-Steady Approach

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    Aerodynamic Analysis of Flexible Flapping Wing Micro Aerial Vehicle Using Quasi-Steady Approach

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    Document information
    Title:

    Aerodynamic Analysis of Flexible Flapping Wing Micro Aerial Vehicle Using Quasi-Steady Approach

    Contributors:

    Vijayakumar, Kolandapaiyan (author) / Chandrasekhar, Uttam (author) / Chandrashekhar, Nagaraj (author)

    Published in:

    Journal of the Institution of Engineers (India) / C ; 97

    Publication date:

    2016

    ISSN:

    2250-0545

    DOI:

    https://doi.org/10.1007/s40032-016-0230-4

    Type of media:

    Article (Journal)

    Type of material:

    Print

    Language:

    English

    Keywords:

    Computational fluid dynamics (CFD) , MATLAB , Aerodynamics , Wind tunnel test , Quasi-steady approach

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