A simplified compound-pendulum method for the experimental determination of the moments of inertia of airplanes about the x and y axes is described. The method is developed as a modification of the standard pendulum method reported previously in NACA report, NACA-467. A brief review of the older method is included to form a basis for discussion of the simplified method. (author)


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    Titel :

    The experimental determination of the moments of inertia of airplanes by a simplified compound-pendulum method


    Beteiligte:

    Erscheinungsdatum :

    01.06.1948


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch