Search U.S. government technical reports digitized or harvested by TRAIL.
Wind tunnel force tests in wing systems through large angles of attack
Wind Tunnel Pressure Distribution Tests on an Airfoil With Trailing Edge Flap
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
Resume of Air-Load Data on Slats and Flaps
Tests of Round and Flat Spoilers on a Tapered Wing in the NACA 19-Foot Pressure Wind Tunnel