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1951

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 Wed Oct 22 02:00:54 2014 PDT.