Add to ORKGWind tunnel tests were conducted in the Langley 7 x 10 foot wind tunnel at Mach numbers less than 0.20 and at Reynolds numbers less than 3.74 million. The effect of the aft area on the 45 deg swept wing longitudinal aerodynamic characteristics at low subsonic speeds and at an angle of attack range from approximately -2 deg to 28 deg was studied. The data are presented without analysis
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
The Langley full scale tunnel was used to investigate the low speed stability and control of an adva...
The longitudinal aerodynamic characteristics of a wing-body-horizontal-tail configuration designed f...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...
An investigation was conducted in the Langley low turbulence pressure tunnel to determine the effect...
A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-s...
Wind tunnel test results have been presented herein for a subsonic transport type wing fitted with w...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
A summary and analysis have been made of the results of various investigations to determine the aero...
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel to determine the longitudinal...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
The Langley full scale tunnel was used to investigate the low speed stability and control of an adva...
The longitudinal aerodynamic characteristics of a wing-body-horizontal-tail configuration designed f...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the static longitu...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
The low speed aerodynamic characteristics of a large-scale model intended to represent advanced fixe...
Results are presented of wind-tunnel tests made at low speed of various small-scale models of sweptb...
A low speed wind tunnel test was conducted in the Langley V/STOL tunnel to determine the static long...
An investigation was conducted in the Langley low turbulence pressure tunnel to determine the effect...
A wind-tunnel investigation was conducted in the Langley 12-Foot Low-Speed Tunnel to study the low-s...
Wind tunnel test results have been presented herein for a subsonic transport type wing fitted with w...
Results of a low-speed wind-tunnel investigation to determine the effect of high-lift devices on the...
A summary and analysis have been made of the results of various investigations to determine the aero...
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel to determine the longitudinal...
A wind tunnel investigation was conducted in the Langley 12-Foot Low-Speed Wind Tunnel to study the ...
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees...
The Langley full scale tunnel was used to investigate the low speed stability and control of an adva...