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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 aerodynamic characteristics of a slotted Clark y wing as affected by the auxiliary airfoil position

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

The Effects of Full-Span and Partial-Span Split Flaps on the Aerodynamic Characteristics of a Tapered Wing

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

Wind-tunnel investigation of rectangular and tapered NACA 23012 wings with plain ailerons and full-span split flaps

Wind-Tunnel Investigation of an N.A.C.A. 23012 Airfoil with a Slotted Flap and Three Types of Auxiliary Flap

Pressure Distribution Over an NACA 23012 Airfoil With an NACA 23012 External-Airfoil Flap

Wind-Tunnel of Three Lateral-Control Devices in Combination With a Full-Span Slotted Flap on an NACA 23012 Airfoil

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 an N.A.C.A. 23012 Airfoil with a Slotted Flap and Three Types of Auxiliary Flap

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

Resume of Air-Load Data on Slats and Flaps


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