Unsteady vorticity–streamfunction algorithm for external flows

A non-inertial vorticity–streamfunction algorithm of the Reynolds-averaged Navier–Stokes equations is developed for studying unsteady and turbulent flows past airfoils. The equations are solved on a non-orthogonal C-grid using a combined finite-difference/finite-volume technique. Comparative computa...

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Published inComputers & fluids Vol. 30; no. 1; pp. 69 - 87
Main Authors Sørensen, Jens N., Nygreen, Per J.
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.09.2000
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ISSN0045-7930
1879-0747
DOI10.1016/S0045-7930(00)00004-9

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Abstract A non-inertial vorticity–streamfunction algorithm of the Reynolds-averaged Navier–Stokes equations is developed for studying unsteady and turbulent flows past airfoils. The equations are solved on a non-orthogonal C-grid using a combined finite-difference/finite-volume technique. Comparative computations are carried out employing three different turbulence models. These are the algebraic zero-equation model of Baldwin and Lomax [1], and the one-equation models of Baldwin and Barth [2] and Spalart and Allmaras [3]. The performance of the models is evaluated against experiments of the Aérospatiale-A airfoil at incidences up to 40° and against two cases of an oscillating NACA 0015 airfoil experiencing light and deep stall. The computations demonstrate that the vorticity–streamfunction formulation combined with standard eddy-viscosity turbulence models is capable of predicting accurately unsteady and turbulent flows past airfoils.
AbstractList A non-inertial vorticity-streamfunction algorithm of the Reynolds-averaged Navier-Stokes equations is developed for studying unsteady and turbulent flows past airfoils. The equations are solved on a non-orthogonal C-grid using a combined finite-difference/finite-volume technique. Comparative computations are carried out employing three different turbulence models. These are the algebraic zero-equation model of Baldwin and Lomax, and the one-equation models of Baldwin and Barth and Spalart and Allmaras. The performance of the models is evaluated against experiments of the Aerospatiale-A airfoil at incidences up to 40 degree and against two cases of an oscillating NACA 0015 airfoil experiencing light and deep stall. The computations demonstrate that the vorticity-streamfunction formulation combined with standard eddy-viscosity turbulence models is capable of predicting accurately unsteady and turbulent flows past airfoils.
A non-inertial vorticity–streamfunction algorithm of the Reynolds-averaged Navier–Stokes equations is developed for studying unsteady and turbulent flows past airfoils. The equations are solved on a non-orthogonal C-grid using a combined finite-difference/finite-volume technique. Comparative computations are carried out employing three different turbulence models. These are the algebraic zero-equation model of Baldwin and Lomax [1], and the one-equation models of Baldwin and Barth [2] and Spalart and Allmaras [3]. The performance of the models is evaluated against experiments of the Aérospatiale-A airfoil at incidences up to 40° and against two cases of an oscillating NACA 0015 airfoil experiencing light and deep stall. The computations demonstrate that the vorticity–streamfunction formulation combined with standard eddy-viscosity turbulence models is capable of predicting accurately unsteady and turbulent flows past airfoils.
Author Nygreen, Per J.
Sørensen, Jens N.
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Keywords Navier–Stokes equations
vorticity–streamfunction
Unsteady flow
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Snippet A non-inertial vorticity–streamfunction algorithm of the Reynolds-averaged Navier–Stokes equations is developed for studying unsteady and turbulent flows past...
A non-inertial vorticity-streamfunction algorithm of the Reynolds-averaged Navier-Stokes equations is developed for studying unsteady and turbulent flows past...
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SubjectTerms Algorithms
Finite difference method
Finite volume method
Navier Stokes equations
Turbulent flow
Unsteady flow
Viscosity
Vortex flow
vorticity–streamfunction
Title Unsteady vorticity–streamfunction algorithm for external flows
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