Desai, SS (1994) Viscous flow past aerofoils axisymmetric bodies and wings 13; 13;. In: CFD: Advances and Applications, 1994, India.
Full text not available from this repository.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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