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Davidson, Harold William (1951) Lift Increase Obtained with Boundary Layer Suction on a 10% Double Wedge Airfoil with a 20% Chord Leading and Trailing Edge Flaps. Engineer's thesis, California Institute of Technology. doi:10.7907/KPZ6-2V51. https://resolver.caltech.edu/CaltechETD:etd-03192009-110707

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