Numerical Studies on an Active Flow Circulation Controlled Flap Concept for Aeronautical Applications

Four different circulation controlled airfoils have been numerically simulated. The baseline airfoil was a 17% thick supercritical airfoil. Different blowing rates have been examined by adjusting the slot height and blowing velocity. A number of turbulence models were employed, these were: Spalart-A...

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Veröffentlicht in:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 2006, Vol.49(163), pp.25-30
Hauptverfasser: ZACHAROS, Athanasios, KONTIS, Konstantinos
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Sprache:eng
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