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title: National Advisory Committee for Aeronautics -- Reports
Pressure distribution over airfoil section with flap and tab
Wind-tunnel investigation of N.A.C.A. 23021 airfoil with various arrangements of slotted flaps
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
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 rectangular airfoil with partial-span split flap
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 research comparing lateral control devices, particularly at high angles of attack -- XII
Wind-tunnel tests of clark Y wing having split flaps with gaps
Wind-tunnel tests of clark Y wing having split flaps with gaps
Effect of partial-span split flaps on aerodynamic characteristics of clark Y wing
Wind tunnel pressure distribution tests on an airfoil with trailing edge flap
Pressure distribution over clarke Y-H airfoil section with split flap
Pressure distribution over clarke Y-H airfoil section with split flap