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Drag reduction effect by uniform blowing on the pressure surface of an airfoil is investigated through wind-tunnel experiments. The measurement result indicates that the total drag is reduced by UB about 5%, although the measurement uncertainty is estimated to be on the same order.
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This page is a summary of: Drag Reduction by Uniform Blowing on the Pressure Surface of an Airfoil, AIAA Journal, November 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j060831.
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