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Jump to: 1951 Number of items: 1. 1951Davidson, 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 |