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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    Titel :

    Airplane control surface


    Weitere Titelangaben:

    Soc Nav Architects Japan -- Advance Paper



    Erscheinungsdatum :

    1931


    Format / Umfang :

    11 pages


    Anmerkungen:

    1 Supp plate


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Japanisch




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