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title: National Advisory Committee for Aeronautics -- Reports
Pressure distribution over NACA 23012 airfoil with fixed slot and slotted flap
Wind-tunnel investigation of N.A.C.A. 23021 airfoil with various arrangements of slotted flaps
Pressure distribution over rectangular airfoil with partial-span split flap
Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap
Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flap
Pressure distribution over NACA 23021 airfoil with slotted and split flap
Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps
Wind-tunnel investigation of aerodynamic balancing of upper-surface ailerons and split flaps
Pressure distribution over airfoil section with flap and tab
Wind-tunnel research comparing lateral control devices, particularly at high angles of attack
Wind tunnel research comparing lateral control devices, particularly at high angles of attack -- XII
Wind-tunnel investigation of N.A.C.A. 23012 airfoil with various arrangements of slotted flaps
Characteristics of Clark Y wing model equipped with several forms of low-drag fixed slots
Aerodynamic characteristics of slotted clark Y wing as affected by auxiliary airfoil position
Wind-tunnel investigation of NACA 23012 airfoil with two sizes of balanced split flap