Account of investigation to determine pressure distribution over two horizontal tail surfaces in uniform free flight. n 119 1921 40 pp. 85 figs, Shows that results obtained upon model tail surfaces can be used to accurately predict loads upon full-sized tail and also to find distribution of load when large elevator angles are used. n 148 1922 26 pp. 33 figs., deals with distribution of pressure during accelerated flight of full-sized airplane, for purpose of determining magnitude of tail and fuselage stresses in stunting.


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    Titel :

    The pressure distribution over the horizontal tail surfaces of an airplane


    Weitere Titelangaben:

    Nat. Advisory Committee Aeronautics, report



    Erscheinungsdatum :

    1921


    Anmerkungen:

    4 figs


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :