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Pressure Distribution Over a Thick, Tapered and Twisted Monoplane Wing Model-N.A.C.A. 81-J
The vertical wind tunnel of the National Advisory Committee for Aeronautics
The Effect of Partial-Span Split Flaps on the Aerodynamic Characteristics of a Clark Y Wing
Resume of Present Data on Load Distribution on Slots and Flaps, Special Report
Wind-Tunnel Measurements of Air Loads on Split Flaps
Wind-Tunnel Investigation of the Aerodynamic Balancing of Upper-Surface Ailerons and Split Flaps
Wind-Tunnel Investigation of Ordinary and Split Flaps on Airfoils of Different Profile
Pressure Distribution Over an Airfoil Section With a Flap and Tab
Notes on Factors Affecting Geometrical Arrangement of Tricycle-Type Landing Gears
Pressure Distribution Over Airfoils With Fowler Flaps
Wind-Tunnel Investigation of Tapered Wings With Ordinary Ailerons and Partial-Span Split Flaps
Pressure Distribution Over a Clark Y-H Airfoil Section With a Split Flap
Pressure distribution over a rectangular airfoil with a partial-span split flap
Pressure Distribution Over an NACA 23012 Airfoil With an NACA 23012 External-Airfoil Flap
Wind-Tunnel Tests of a Clark Y Wing Having Split Flaps With Gaps
Pressure distribution over an NACA 23012 airfoil with a slotted and a plain flap
Wind-Tunnel Investigation of an NACA 23012 Airfoil with Various Arrangements of Slotted Flaps
Wind-tunnel investigation of NACA 23012 airfoil with various arrangements of slotted flaps
Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils with various sizes of split flap