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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. http://resolver.caltech.edu/CaltechETD:etd-03192009-110707

This list was generated on Fri Nov 28 02:00:53 2014 PST.