In this work elevator effectiveness for tandem-scheme aircraft (unmanned aerial vehicle or piloted one) is considered. Presented mathematical models take into account the changing of zero-lift pitching moment coefficient and wing-wing aerodynamic interference. It allows choosing geometrical parameters of flight controls for aircraft under design.


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    Title :

    Tandem-Scheme Aircraft Controllability


    Contributors:


    Publication date :

    2019-10-01


    Size :

    412556 byte



    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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