CONSIDER a single rotor helicopter disturbed from the hovering condition as in FIG. 16. It has acquired a small forward velocity V ft./sec. and a nose-up angular velocity of q rads./sec. For simplicity we consider the centre of gravity of the fuselage to be on the shaft axis, since its actual position can be shown to have a negligible effect in hovering. Resolving moments about the centre of gravity, the important terms are


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Helicopter Longitudinal Stability


    Untertitel :

    Some Contributions to Existing Theory


    Beteiligte:
    Payne, P.R. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1957-06-01


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Helicopter Longitudinal Stability

    Payne, P.R. | Emerald Group Publishing | 1957


    Helicopter longitudinal stability

    Payne, P.R. | Engineering Index Backfile | 1957



    Method for studying helicopter longitudinal maneuver stability

    Amer, K.B. | Engineering Index Backfile | 1954