A Viscous-Inviscid Interaction Model for Rotor Aerodynamics

Antonino Filippone, Jens Nørkær Sørensen

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    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
    Publication date1994
    Publication statusPublished - 1994
    EventAerodynamics and Aeroacustics of Rotorcraf - Berlin
    Duration: 1 Jan 1994 → …


    ConferenceAerodynamics and Aeroacustics of Rotorcraf
    Period01/01/1994 → …

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