Flight tests, force tests, and damping in roll tests were made on model with wing set at angles of skew from 0° to 60°; investigation was of exploratory nature and was intended to provide only preliminary and qualitative indication of whether such design could be flown.


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    Titel :

    Investigation of stability and control characteristics of airplane model with skewed wing in Langley freeflight tunnel


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Note


    Beteiligte:
    Campbell, J.P. (Autor:in) / Drake, H.M. (Autor:in)


    Erscheinungsdatum :

    1947


    Format / Umfang :

    13 pages


    Anmerkungen:

    Supp Sheets


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :