Evaluation for small single rotor helicopter with various types of control feedback; effects of fuselage pitching moment characteristics on stability also evaluated; problem of maintaining stability with respect to velocity at high forward speeds.


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    Titel :

    Helicopter longitudinal stability in forward flight with control feedback and fuselage aerodynamics


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Wernicke, K.G. (Autor:in)


    Erscheinungsdatum :

    1957


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Aerodynamics of helicopter in forward flight

    Brailsford, E.N. | Engineering Index Backfile | 1956



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    Numerical Prediction of Canard-Fuselage Interaction for a Helicopter in a Helicopter in Forward Flight

    Aslan, A. R. / Gulcat, U. / Asian Fluid Mechanics Committee | British Library Conference Proceedings | 1995