It is claimed, in present practice, that control surfaces are designed with risks, relying upon experience of designers and judgement of test pilots; angular velocity with which airplane rotates corresponding to maximum rudder angle when it flies with minimum velocity, is calculated for recent airplanes; control surfaces should be so designed that angular velocity is greater than mean value for category to which airplane belongs.


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    Title :

    Airplane control surface


    Additional title:

    Soc Nav Architects Japan -- Advance Paper



    Publication date :

    1931


    Size :

    11 pages


    Remarks:

    1 Supp plate


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    Japanese




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