Calculation of a Helicopter Rotor in Hover by Viscous-Inviscid Interaction

Antonino Filippone, Jens Nørkær Sørensen

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    Abstract

    A viscous inviscid interaction model has been developed for the calculation of steady and unsteady aerodynamic flows. The model is validfor two-dimensional and three-dimensional flows alike. We use a fully three-dimensional boundary element method as inviscid flow model, and a two-dimensional or quasi three-dimensionalformulation of the Navier-Stokes equations invorticity-velocity variables for the viscous flow.
    Original languageEnglish
    Title of host publication13th AIAA Applied Aerodynamics Conference
    Place of PublicationWashington
    PublisherAIAA
    Publication date1995
    Publication statusPublished - 1995
    Event13th AIAA Applied Aerodynamics Conference - San Diego, CA
    Duration: 1 Jan 1995 → …

    Conference

    Conference13th AIAA Applied Aerodynamics Conference
    CitySan Diego, CA
    Period01/01/1995 → …

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