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    Title :

    Comparison between dynamic stability boundaries for NPL 9615 and NACA 0012 aerofoils pitching about the quarter-chord


    Contributors:


    Publication date :

    1974


    Size :

    29 S., [12] Bl.


    Remarks:

    graph. Darst.
    Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek


    Type of media :

    Book


    Type of material :

    Print


    Language :

    English



    Classification :

    BKL:    50.34 Gasdynamik, Aerodynamik / 55.50 Luftfahrzeugtechnik



    NPL 9615 and NACA 0012 - a comparison of aerodynamic data

    Gregory, N. / Wilby, P. G. | TIBKAT | 1973


    Numerical Simulation of a Pitching NACA 0012 Airfoil

    Pechloff, A. / International Council of the Aeronautical Sciences | British Library Conference Proceedings | 2000


    Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil

    Pruski, Brandon / Humble, Raymond / Bowersox, Rodney | AIAA | 2011


    Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil

    Pruski, B. J. / Bowersox, R. D. W. | AIAA | 2013