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Pressure distribution over NACA 23012 airfoil with a slotted and a split flap

Wind-tunnel investigation of an NACA 23012 airfoil with two sizes of balanced split flap

Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils equipped with 40-percent-chord double slotted flaps

Pressure distribution over an NACA 23012 airfoil with a fixed slot and a slotted flap

Wind-tunnel investigation of plain ailerons for a wing with a full-span flap consisting of an inboard Fowler and an outboard retractable split flap


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