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.
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|
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