A Viscous-Inviscid Interaction Model for Rotor Aerodynamics

Antonino Filippone, Jens Nørkær Sørensen

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    Abstract

    A numerical model for the viscous-inviscid interactive computations ofrotor flows is presented. The basic methodology for deriving the outer inviscid solution is a fully three-dimensional boundary element method.The inner viscous domain, i.e. the boundary layer, is described by the two-dimensional Navier-Stokes equations
    Original languageEnglish
    Title of host publicationAerodynamics and Aeroacustics of Rotorcraf
    Place of PublicationParis
    PublisherAGARD
    Publication date1994
    Publication statusPublished - 1994
    Event75th Fluid Dynamics Symposium: Aerodynamics and Aeroacoustics of Rotorcraft - Berlin, Germany
    Duration: 10 Oct 199413 Oct 1994

    Conference

    Conference75th Fluid Dynamics Symposium
    Country/TerritoryGermany
    CityBerlin
    Period10/10/199413/10/1994

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