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 29
10 -10 0 10 -10 0 Angle of attack, cL , degrees Figtire 10.- Comparison of computed- and. observed characteristics for simple split flaps on a Clark Y wing.
NASA Technical Reports Server (NTRS)
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