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A low speed wind tunnel investigation is presented documenting the effect of leading and trailing edge flaps on a flat plate. The results show that these airfoils have low sensitivity to Reynolds number and exceed the efficiency of circular arc profiles.
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This page is a summary of: Efficient Low-Reynolds-Number Airfoils, Journal of Aircraft, September 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035515.
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