Add to ORKGWind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with external flow jet fla
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel and in a scaled version of th...
An investigation has been conducted to determine the effects of flap span and wing aspect ratio on t...
The flight test program objectives are: (1) To determine the in-flight aerodynamic, performance, and...
The stability and control characteristics of a four-engine turbofan STOL transport model having an e...
Wind tunnel tests of large jet transport aircraft model with external flow jet fla
Wind tunnel investigation of jet transport airplane configuration with high thrust-weight ratio and ...
The low speed longitudinal characteristics of the jet flap STOL model were determined. The 17 percen...
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...
Effect of engine position and high lift devices on aerodynamic characteristics of external flow, jet...
Wind tunnel investigation of jet transport airplane configuration with external flow jet flap and in...
Determination of low speed longitudinal aerodynamic characteristics of four engine externally blowin...
The model tested was a general research model of a swept-wing, jet-powered STOL transport with exter...
An investigation of the static longitudinal aerodynamic characteristics of a semispan STOL jet trans...
An investigation was conducted to determine the aerodynamic characteristics of a large-scale subsoni...
A wind tunnel investigation was made of the aerodynamic characteristics of a 14.5 foot semispan, ext...
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel and in a scaled version of th...
An investigation has been conducted to determine the effects of flap span and wing aspect ratio on t...
The flight test program objectives are: (1) To determine the in-flight aerodynamic, performance, and...
The stability and control characteristics of a four-engine turbofan STOL transport model having an e...
Wind tunnel tests of large jet transport aircraft model with external flow jet fla
Wind tunnel investigation of jet transport airplane configuration with high thrust-weight ratio and ...
The low speed longitudinal characteristics of the jet flap STOL model were determined. The 17 percen...
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...
Effect of engine position and high lift devices on aerodynamic characteristics of external flow, jet...
Wind tunnel investigation of jet transport airplane configuration with external flow jet flap and in...
Determination of low speed longitudinal aerodynamic characteristics of four engine externally blowin...
The model tested was a general research model of a swept-wing, jet-powered STOL transport with exter...
An investigation of the static longitudinal aerodynamic characteristics of a semispan STOL jet trans...
An investigation was conducted to determine the aerodynamic characteristics of a large-scale subsoni...
A wind tunnel investigation was made of the aerodynamic characteristics of a 14.5 foot semispan, ext...
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel and in a scaled version of th...
An investigation has been conducted to determine the effects of flap span and wing aspect ratio on t...
The flight test program objectives are: (1) To determine the in-flight aerodynamic, performance, and...