Unsteady-lift functions for wings of finite aspect ratio have been calculated by correcting the aerodynamic inertia and the angle of attack of the infinite wing. The calculations are based on the operational method.


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    Titel :

    The unsteady lift of a wing of finite aspect ratio


    Beteiligte:

    Erscheinungsdatum :

    01.01.1940


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Unsteady lift of wing of finite aspect ratio

    Jones, R.T. | Engineering Index Backfile | 1940


    Unsteady lift of finite wing

    Jones, R.T. | Engineering Index Backfile | 1939


    The unsteady lift of a finite wing

    Jones, Robert T. | SLUB | 1938


    The unsteady lift of a finite wing

    Jones, Robert T. | TIBKAT | 1938