A resume of the equations and formulas for the forces and moments on an aircraft-engine mount is presented. In addition, available experimental data have been included to permit the computation of these forces and moments. A sample calculation is made and compared with present design conditions for engine mounts.


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    Titel :

    The forces and moments on airplane engine mounts


    Beteiligte:
    Donely, Philip (Autor:in)

    Erscheinungsdatum :

    1936-12-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



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