Computational investigation of incompressible airfoil flows at high angles of attack

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Author
Mathre, John Mark
Date
1988-12Advisor
Platzer, Max F.
Second Reader
Howard, R.M.
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Show full item recordAbstract
Cebeci's viscous/inviscid interaction program was applied
to the analysis of steady, two dimensional, incompressible
flow past four airfoils, the NACA 66₃-018, 0010 (Modified),
4412 and the Wortmann FX 63-137. Detailed comparisons with
the available experimental results show that the essential
features are correctly modelled, but that significant
discrepancies are found in regions of flow separations.