Unsteady RANS simulation of incompressible flow past a symmetric aerofoil at high angles of attack
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Unsteady RANS simulation of incompressible flow past a symmetric aerofoil at high angles of attack
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| Creator |
Majumdar, Sekhar
Rajani, BN Kulkarni, DS Subrahmanya, MB |
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| Subject |
Fluid Mechanics and Thermodynamics
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| Description |
Turbulent flow past a stationary NACA0012 aerofoil at high angle of attack is analysed solving the Unsteady Reynolds Averaged Navier Stokes (URANS) equations coupled to different eddy viscosity based turbulence models. The complex phenomena of vortex shedding for stationary aerofoil at very high angles of attack has been reasonably captured by the present method.
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| Type |
Conference or Workshop Item
PeerReviewed |
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| Format |
application/pdf
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| Identifier |
http://nal-ir.nal.res.in/11770/1/2%2D12th%2DACFM%2DKorea%2DRajani%2DAug%2D2008.pdf
Majumdar, Sekhar and Rajani, BN and Kulkarni, DS and Subrahmanya, MB Unsteady RANS simulation of incompressible flow past a symmetric aerofoil at high angles of attack. In: Proceedings of the 12th Asian Congress of Fluid Mechanics, August 18-21, 2008, Daejeon, Korea. |
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| Relation |
http://nal-ir.nal.res.in/11770/
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