Investigation of Boundary-layer Control to Improve the Lift and Drag Characteristics of the NACA 65₂-415 Airfoil Section with Double Slotted and Plain Flaps
Description:
From summary: "A two-dimensional wind-tunnel investigation has been made of the relative effectiveness of two methods of boundary-layer control in increasing the maximum lift coefficient of an NACA 652-415 airfoil section."
Date:
August 1950
Creator:
Horton, Elmer A.; Racisz, Stanley Frank & Paradiso, Nicholas J.
Item Type:
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Partner:
UNT Libraries Government Documents Department