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    Titel :

    Theoretical Investigations of a Helicopter Rotor in Steep Descent


    Beteiligte:
    Chen, Chang (Autor:in) / Prasad, J.V.R. (Autor:in)

    Kongress:

    AIAA Modeling and Simulation Technologies Conference and Exhibit



    Erscheinungsdatum :

    01.01.2005




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    HELICOPTER MAIN ROTOR AERODYNAMIC PERFORMANCE IN DESCENT CONDITIONS

    Anikin, V. / American Helicopter Society | British Library Conference Proceedings | 2002


    Flow through a helicopter rotor in vertical descent

    Brotherhood, P. / Aeronautical Research Council | TIBKAT | 1952


    A Simplified Inflow Model of a Helicopter Rotor in Vertical Descent

    Chen, C. / Prasad, J. V. R. / Basset, P.-M. et al. | British Library Conference Proceedings | 2004


    EXPERIMENTAL AND THEORETICAL INVESTIGATIONS TO DEVELOP A MODEL OF ROTOR AERODYNAMICS ADAPTED TO STEEP DESCENTS

    Taghizad, A. / Jimenez, J. / Binet, L. et al. | British Library Conference Proceedings | 2002


    Steep-Descent Maneuver of Transport Aircraft

    Antonio Filippone | AIAA | 2007