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The Computation of Viscid-Inviscid Interaction on Airfoils with Separated Flow

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Numerical and Physical Aspects of Aerodynamic Flows III

Abstract

In this paper we are concerned with the computation of viscous subsonic and transonic flow over two-dimensional airfoils at high Reynolds numbers where the boundary layers are thin and turbulent over most of the airfoil and wake. Our objective in this work is to develop a fast viscid-inviscid-interaction method that can compute viscous flows over airfoils with extensive regions of flow separation and that can be used to predict the stalling characteristics of airfoils with reasonable accuracy.

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© 1986 Springer-Verlag New York Inc.

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Melnik, R.E., Brook, J.W. (1986). The Computation of Viscid-Inviscid Interaction on Airfoils with Separated Flow. In: Cebeci, T. (eds) Numerical and Physical Aspects of Aerodynamic Flows III. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-4926-9_5

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  • DOI: https://doi.org/10.1007/978-1-4612-4926-9_5

  • Publisher Name: Springer, New York, NY

  • Print ISBN: 978-1-4612-9362-0

  • Online ISBN: 978-1-4612-4926-9

  • eBook Packages: Springer Book Archive

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