Abstract A possibility of using the main rotor in designing a vertical takeoff and landing aircraft with a disk wing is analyzed. We propose integrating the main rotor and a disk wing for solving some problems of main rotors.


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    Titel :

    Disk wing as a solution of some “eternal” problems of main rotor


    Beteiligte:
    Pavlov, V. A. (Autor:in) / Pavlov, V. V. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2012-01-01


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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