Two flight conditions examined, high speed level flight and pullup maneuvers; in both conditions, retreating tip angles of attack as high as 6° or 7° beyond stall value are encountered; pertinence to problem of increased periodic control loads in future helicopters. See also NACA -- Tech Note 4203 separately indexed.


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    Titel :

    Flight investigation of effects of retreating-blade stall on bending and torsional moments encountered by helicopter rotor blade


    Weitere Titelangaben:

    NACA -- Tech Note


    Beteiligte:
    Ludi, L.H. (Autor:in)


    Erscheinungsdatum :

    1958


    Format / Umfang :

    23 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :