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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    13 pages


    Remarks:

    Supp Sheets


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :