Tests to determine rolling moment, yawing moment, hinge moment and effect of midchord wing slots on characteristics of wing and aileron and tab; effect of leakage around tab hinge.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Investigation of aileron and tab of spring-tab lateral-control system in Langley 19-foot pressure tunnel


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    34 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English