Add to ORKGLateral control & hinge moment of spoiler-slot- deflector on sweptback wing at subsonic spee
Flow spoiler and aerodynamic balance effects on oscillating hinge moments for swept fin-rudder combi...
An investigation has been made at a Mach nuniberof 1.61 snd a Reynolds nw?iberof 4.2 X 106 to determ...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach number...
Aerodynamic characteristics of variable-wing-sweep configuration with spoiler-slot-deflector control...
Wind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control syste
Pressure distributions and aerodynamic characteristics of spoiler-type controls on trapezoidal wing ...
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
Tests of a partial-span model of a large bomber-type air1ane were conducted to determine the. aerody...
Roll-control effectiveness of spoiler configurations on aircraft model with variable sweep wings at ...
Tests of a partial-span model of a large bomber-type air1ane\ud were conducted to determine the. aer...
This paper present results of an investigation of the lateral-control and hinge-moment characteristi...
Wind tunnel study to explore use of slot spoilers for direct control of flap induced lift and latera...
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...
Flow spoiler and aerodynamic balance effects on oscillating hinge moments for swept fin-rudder combi...
An investigation has been made at a Mach nuniberof 1.61 snd a Reynolds nw?iberof 4.2 X 106 to determ...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach number...
Aerodynamic characteristics of variable-wing-sweep configuration with spoiler-slot-deflector control...
Wind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control syste
Pressure distributions and aerodynamic characteristics of spoiler-type controls on trapezoidal wing ...
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
Tests of a partial-span model of a large bomber-type air1ane were conducted to determine the. aerody...
Roll-control effectiveness of spoiler configurations on aircraft model with variable sweep wings at ...
Tests of a partial-span model of a large bomber-type air1ane\ud were conducted to determine the. aer...
This paper present results of an investigation of the lateral-control and hinge-moment characteristi...
Wind tunnel study to explore use of slot spoilers for direct control of flap induced lift and latera...
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...
Flow spoiler and aerodynamic balance effects on oscillating hinge moments for swept fin-rudder combi...
An investigation has been made at a Mach nuniberof 1.61 snd a Reynolds nw?iberof 4.2 X 106 to determ...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...