Basis and extent of theoretical induced velocity calculations; theory applied to interference problems involving additional rotors, wings, and tails in flow; for hovering, superposition is used to introduce ground effect into calculations; it is concluded that present induced flow theory cannot be used to predict detailed aerodynamic loading on rotor blades. See also Engineering Index 1957 p 512.


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    Titel :

    Induced flow near helicopter rotor


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Heyson, H.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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