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Showing 1 to 1 of 1 for “"trailing edge plain flap"”.
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Experimental wind tunnel study of airfoils with large flap deflections at low Reynolds numbers
… at low Reynolds numbers for four airfoils with trailing edge plain flaps in an attempt to understand the effects of Reynolds number, percent thickness (t/c), percent chord of flap (flap-chord ratio), and flap deflection on airfoil performance. The four airfoils used in this research were the …