Investigation made in Langley 7- by 10-foot tunnel; results indicate peak pressures on plug type spoiler slot aileron that may result in compressibility shock on plug aileron at high speed; max loads on plug aileron occurred in high speed condition for maximum up aileron deflection.


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    Title :

    Pressure distribution over plug-type spoiler-slot aileron on tapered wing with full-span slotted flaps


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:
    Lowry, J.G. (author) / Turner, T.R. (author)


    Publication date :

    1946


    Size :

    10 pages


    Remarks:

    Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :