Two families of airfoil sections which can be used for helicopter/rotorcraft rotor blades or aircraft propellers of a particular shape are prepared. An airfoil of either family is one which could be produced by the combination of a camber line and a thickness distribution or a thickness distribution which is scaled from these. An airfoil of either family has a unique and improved aerodynamic performance. The airfoils of either family are intended for use as inboard sections of a helicopter rotor blade or an aircraft propeller.


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    Titel :

    High Lift, Low Pitching Moment Airfoils


    Beteiligte:

    Erscheinungsdatum :

    1988-10-11


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    High-Lift, Low-Pitching-Moment Airfoils

    Noonan, Kevin W. | NTRS | 1987




    Lift Enhancement of High Angle of Attack Airfoils Using Periodic Pitching

    Dawson, Scott T. / Hemati, Maziar / Floryan, Daniel C. et al. | AIAA | 2016