Theoretical study demonstrating that control force of ordinary ailerons may be reduced to zero over range of deflections and at given flight condition by use of appropriate differential movement; approximates to ideal motion obtainable with simple linkage; chart for selection of appropriate crank arrangement; practical application of system.


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    Title :

    Reduction of aileron operating force by differential linkage


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Notes


    Contributors:
    Jones, R.T. (author) / Nerken, A.I. (author)


    Publication date :

    1936


    Size :

    13 pages


    Remarks:

    10 Supp sheets, Bibliography


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English