A Viscous-Inviscid Interaction Model for Rotor Aerodynamics

Antonino Filippone; Jens Nørkær Sørensen

A Viscous-Inviscid Interaction Model for Rotor Aerodynamics

Antonino Filippone, Jens Nørkær Sørensen

Research output: Chapter in Book/Report/Conference proceeding › Article in proceedings › Research › peer-review

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 language	English
Title of host publication	Aerodynamics and Aeroacustics of Rotorcraf
Place of Publication	Paris
Publisher	AGARD
Publication date	1994
Publication status	Published - 1994
Event	Aerodynamics and Aeroacustics of Rotorcraf - Berlin Duration: 1 Jan 1994 → …

Conference

Conference	Aerodynamics and Aeroacustics of Rotorcraf
City	Berlin
Period	01/01/1994 → …

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Cite this

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title = "A Viscous-Inviscid Interaction Model for Rotor Aerodynamics",

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",

author = "Antonino Filippone and S{\o}rensen, {Jens N{\o}rk{\ae}r}",

year = "1994",

language = "English",

booktitle = "Aerodynamics and Aeroacustics of Rotorcraf",

publisher = "AGARD",

note = "Aerodynamics and Aeroacustics of Rotorcraf ; Conference date: 01-01-1994",

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AU - Filippone, Antonino

AU - Sørensen, Jens Nørkær

PY - 1994

Y1 - 1994

N2 - 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

AB - 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

M3 - Article in proceedings

BT - Aerodynamics and Aeroacustics of Rotorcraf

PB - AGARD

CY - Paris

T2 - Aerodynamics and Aeroacustics of Rotorcraf

Y2 - 1 January 1994

ER -