Static stability and control characteristics of flight test model determined from force tests and lag characteristics of ailerons determined from roll-free stand tests; flight tests of model made through range of lift coefficient from 0.6 through stall by using data obtained from force tests to establish flight test conditions.


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    Title :

    Comparison of lateral controllability with flap and plug ailerons on sweptback-wing model


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    19 pages


    Remarks:

    Diagrs, Charts, Tables


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English