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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Tandem-Scheme Aircraft Controllability


    Beteiligte:


    Erscheinungsdatum :

    01.10.2019


    Format / Umfang :

    412556 byte



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Simulation Analysis of the Controllability of a Tandem Ducted Fan Aircraft

    Tobias, E. / Horn, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008


    Meta Aircraft Controllability

    Troub, Brandon / Montalvo, Carlos J. | AIAA | 2016



    Stability and Controllability of Supersonic Aircraft

    V. Lutskii / E. Galashev | NTIS | 1970