Add to ORKGWind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control syste
This report presents the results of flight tests made to determine the lateral control characteristi...
An investigation was made in the V/STOL tunnel to determine, by the trailing wing sensor technique, ...
A wind-tunnel study has been made to determine the possibility of developing spoilers suitable for p...
Lateral control & hinge moment of spoiler-slot- deflector on sweptback wing at subsonic spee
Aerodynamic characteristics of variable-wing-sweep configuration with spoiler-slot-deflector control...
Wind tunnel study to explore use of slot spoilers for direct control of flap induced lift and latera...
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach number...
Tests of a partial-span model of a large bomber-type air1ane were conducted to determine the. aerody...
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
An airplane stall proofing system utilizing a spoiler was investigated for application on a low wing...
An investigation was conducted in a 300-mph 7- by 10- foot tunnel to obtain data for a slot spoiler ...
In an attempt to find an aerodynamic means of counteracting the transonic trim change of a fighter a...
The longitudinal aerodynamic characteristics of a full scale, single engine general aviation airplan...
A 0.10-scale model of a swept-wing fighter airplane was tested in the Langley high-speed 7- by 10-fo...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
This report presents the results of flight tests made to determine the lateral control characteristi...
An investigation was made in the V/STOL tunnel to determine, by the trailing wing sensor technique, ...
A wind-tunnel study has been made to determine the possibility of developing spoilers suitable for p...
Lateral control & hinge moment of spoiler-slot- deflector on sweptback wing at subsonic spee
Aerodynamic characteristics of variable-wing-sweep configuration with spoiler-slot-deflector control...
Wind tunnel study to explore use of slot spoilers for direct control of flap induced lift and latera...
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach number...
Tests of a partial-span model of a large bomber-type air1ane were conducted to determine the. aerody...
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
An airplane stall proofing system utilizing a spoiler was investigated for application on a low wing...
An investigation was conducted in a 300-mph 7- by 10- foot tunnel to obtain data for a slot spoiler ...
In an attempt to find an aerodynamic means of counteracting the transonic trim change of a fighter a...
The longitudinal aerodynamic characteristics of a full scale, single engine general aviation airplan...
A 0.10-scale model of a swept-wing fighter airplane was tested in the Langley high-speed 7- by 10-fo...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
This report presents the results of flight tests made to determine the lateral control characteristi...
An investigation was made in the V/STOL tunnel to determine, by the trailing wing sensor technique, ...
A wind-tunnel study has been made to determine the possibility of developing spoilers suitable for p...