In this report a theory of thin airfoils of small camber is developed which permits either the velocity distribution corresponding to a given airfoil shape, or the airfoil shape corresponding to a given velocity distribution to be calculated. The procedures to be employed in these calculations are outlined and illustrated with suitable examples.


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    Titel :

    General theory of airfoil sections having arbitrary shape or pressure distribution


    Beteiligte:

    Erscheinungsdatum :

    01.01.1945


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch