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title: National Advisory Committee for Aeronautics -- Reports
Wind-tunnel investigation of N.A.C.A. 23021 airfoil with various arrangements of slotted flaps
Wind-tunnel investigation of N.A.C.A. 23012 airfoil with various arrangements of slotted flaps
Resume of air-load data on slots and 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 tests of clark Y wing having split flaps with gaps
Wind-tunnel tests of clark Y wing having split flaps with gaps
Pressure distribution over airfoils with fowler flaps
Pressure distribution over N.A.C.A. 23012 airfoil with slotted and plain flaps
Pressure distribution over N.A.C.A. 23012 airfoil with N.A.C.A. 23012 external-airfoil 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
Pressure distribution over clarke Y-H airfoil section with split flap
Pressure distribution over clarke Y-H airfoil section with split flap
Resume and analysis of N.A.C.A. lateral control research
Resume and analysis of N.A.C.A. lateral control research
Pressure distribution over rectangular airfoil with partial-span split flap
Pressure distribution over airfoil section with flap and tab
Wind-tunnel tests of wing flaps suitable for direct control of glide-path angle