Viscous flow past aerofoils axisymmetric bodies and wings 13; 13;

Desai, SS (1994) Viscous flow past aerofoils axisymmetric bodies and wings 13; 13;. In: CFD: Advances and Applications, 1994, India.

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Abstract

A brief outline is given here of computing viscous flow past aerospace components such as aerofoils, bodies of revolution and wings, based on a coupling of potential flow computations and integral boundary layer calculations. Direct and semi-inverse procedures for viscous-inviscid coupling are described. Keeping in mind transonic and high Reynolds number flows, only turbulent flow computations are considered; laminar and transitional flows are not covered here.

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: Boundary layer flow;Computational fluid dynamics;Inviscid flow;Potential flow;Turbulent flow;Viscous flow;Axisymmetric bodies;Bodies of revolution;High reynolds number;Wings
Subjects: AERONAUTICS > Aerodynamics
Division/Department: Computational and Theoretical Fluid Dynamics Division
Depositing User: Mrs Manoranjitha M D
Date Deposited: 14 Nov 2006
Last Modified: 24 May 2010 09:52
URI: http://nal-ir.nal.res.in/id/eprint/3175

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