Add to ORKGWind tunnel tests of swept-wing fighter aircraft with spoiler-slot-deflector lateral control system
A wind-tunnel study has been made to determine the possibility of developing spoilers suitable for p...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
Pressure distributions and aerodynamic characteristics of spoiler-type controls on trapezoidal wing ...
Wind tunnel testing of swept wing fighter aircraft model for determining drag and static longitudina...
Wind tunnel test to determine swept wing fighter aircraft drag, and logitudinal and lateral stablity...
Wind tunnel investigations of effect on static stability of modifications to swept wing fighter airc...
Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft
Free flight tunnel testing of swept wing aircraft model to determine roll effectiveness of different...
Low-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small ...
Subsonic and supersonic wind tunnel study of low aspect ratio sweptback wing tailless fighter aircra...
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge sl...
Wind tunnel tests of wingless low aspect ratio folding control missile configurations
Simulated flight tests of elastic swept-wing bomber and fighter model coupled wing tip to wing tip
A wind-tunnel study has been made to determine the possibility of developing spoilers suitable for p...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
Pressure distributions and aerodynamic characteristics of spoiler-type controls on trapezoidal wing ...
Wind tunnel testing of swept wing fighter aircraft model for determining drag and static longitudina...
Wind tunnel test to determine swept wing fighter aircraft drag, and logitudinal and lateral stablity...
Wind tunnel investigations of effect on static stability of modifications to swept wing fighter airc...
Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft
Free flight tunnel testing of swept wing aircraft model to determine roll effectiveness of different...
Low-speed free flight tunnel testing of swept wing fighter aircraft for determining effect of small ...
Subsonic and supersonic wind tunnel study of low aspect ratio sweptback wing tailless fighter aircra...
Results are presented of wind-tunnel investigations at Mach numbers of 0.60 to 0.94 and angles of at...
Wind tunnel tests haved been made at low speed to various small-scale models of swept-back, swept-fo...
Low speed aerodynamic characteristics of swept- wing aircraft with blowing flaps and leading-edge sl...
Wind tunnel tests of wingless low aspect ratio folding control missile configurations
Simulated flight tests of elastic swept-wing bomber and fighter model coupled wing tip to wing tip
A wind-tunnel study has been made to determine the possibility of developing spoilers suitable for p...
Report presents the results of an extensive investigation made in the NACA 7 by 10-foot wind tunnel ...
Pressure distributions and aerodynamic characteristics of spoiler-type controls on trapezoidal wing ...