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A method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y (1936)

NASA Technical Reports Server (NTRS) · leaf 28

An illustration from A method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y, 1936, leaf 28

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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