A three year Cooperative Research Agreements made in each of the three years between the Subsonic Aerodynamics Branch of the NASA Langley Research Center and the Virginia Polytechnic Institute and State University (Va. Tech) has been completed. This document presents results from this three year endeavor. The goal of creating an efficient method to compute unsteady interactional effects between a helicopter rotor and fuselage has been accomplished. This paper also includes appendices to support these findings. The topics are: 1) Rotor-Fuselage Interactions Aerodynamics: An Unsteady Rotor Model; and 2) Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model.


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    Titel :

    Aerodynamic Interaction Effects of a Helicopter Rotor and Fuselage


    Beteiligte:
    D. D. Boyd (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    216 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch