Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    DeYoung, J. (author)


    Publication date :

    1951


    Size :

    71 pages


    Remarks:

    Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :