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

Antonino Filippone; Jens Nørkær Sørensen

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

Antonino Filippone
, Jens Nørkær Sørensen

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

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 language	English
Title of host publication	13th AIAA Applied Aerodynamics Conference
Place of Publication	Washington
Publisher	AIAA
Publication date	1995
Publication status	Published - 1995
Event	13th AIAA Applied Aerodynamics Conference - San Diego, United States Duration: 19 Jun 1995 → 22 Jun 1995 Conference number: 13

Conference

Conference	13th AIAA Applied Aerodynamics Conference
Number	13
Country/Territory	United States
City	San Diego
Period	19/06/1995 → 22/06/1995

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Cite this

@inproceedings{9be38e8ad842440e8c18e09ec1639d83,

title = "Calculation of a Helicopter Rotor in Hover by Viscous-Inviscid Interaction",

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.",

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

year = "1995",

language = "English",

booktitle = "13th AIAA Applied Aerodynamics Conference",

publisher = "AIAA",

note = "13th AIAA Applied Aerodynamics Conference ; Conference date: 19-06-1995 Through 22-06-1995",

}

TY - GEN

T1 - Calculation of a Helicopter Rotor in Hover by Viscous-Inviscid Interaction

AU - Filippone, Antonino

AU - Sørensen, Jens Nørkær

N1 - Conference code: 13

PY - 1995

Y1 - 1995

N2 - 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.

AB - 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.

M3 - Article in proceedings

BT - 13th AIAA Applied Aerodynamics Conference

PB - AIAA

CY - Washington

T2 - 13th AIAA Applied Aerodynamics Conference

Y2 - 19 June 1995 through 22 June 1995

ER -