Abstract The aim of the investigation is to develop a technique of recalculating the lift as a function of the angle of attack at different reference points of the aircraft model height over the ground surface. A technique for evaluating the lift of the aircraft model close to the ground surface is proposed.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Experimental investigation of lift for a wing-in-ground effect aircraft model


    Beteiligte:
    Nazarov, D. V. (Autor:in) / Frolov, V. A. (Autor:in) / Shakhov, V. G. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2016-04-01


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Experimental investigation of lift for a wing-in-ground effect aircraft model

    Nazarov, D. V. / Frolov, V. A. / Shakhov, V. G. | Online Contents | 2016


    High-lift-wing aircraft

    WANG ZHICHENG | Europäisches Patentamt | 2015

    Freier Zugriff

    Tandem wing-connected wing ground effect aircraft

    LU RONGFEI / ZHAO YONGSHENG / ZHOU JIAN et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    HIGH-LIFT DEVICE AND AIRCRAFT WING

    NISHIMURA SHINSUKE | Europäisches Patentamt | 2020

    Freier Zugriff