Test Simulations with the NACA 0012 Airfoil
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Helsinki University of Technology |
J Muu elektroninen julkaisu
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2003
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en
Pages
21
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Abstract
Abstract: Air-flow around the NACA 0012 airfoil was simulated with the FINFLO flow solver version 7.2 of Finflo Ltd. and the 2D solver FINF2D of Laboratory of Aerodynamics, HUT. The flow conditions are Ma = 0.3, α = 10°. Main result: Pressure and friction coefficients are in a good agreement between the two solvers, whereas the drag and lift coefficients have some differencies.Description
MEMO No CFD/THERMO-44-2003
Date: 17th December 2003
Keywords
FINFLO, k-ω model, k-ε model, NACA 0012 Airfoil