Add to ORKGDetermination of low speed longitudinal aerodynamic characteristics of four engine externally blowing jet-flap STOL aircraf
Effect of engine position and high lift devices on aerodynamic characteristics of external flow, jet...
An investigation of the longitudinal aerodynamic characteristics of an aspect ratio 4.735 airfoil ha...
Wind tunnel tests for V/STOL aircraft having direct-lift and lift-cruise jet nozzle
The low speed longitudinal characteristics of the jet flap STOL model were determined. The 17 percen...
Proximity effects of moving ground plane on aerodynamic characteristics of low speed transport aircr...
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the power-on stati...
Wind tunnel investigation of static longitudinal aerodynamic characteristics of semispan swept wing ...
Determination of low speed longitudinal aerodynamic characteristics of four engine externally blowin...
An investigation of the static longitudinal aerodynamic characteristics of a semispan STOL jet trans...
Wind tunnel investigation of jet transport airplane configuration with high thrust-weight ratio and ...
Ground effects investigation of STOL air-sea transport model with blowing over canard and wing flap
A wind-tunnel investigation has been made of the effects of ground proximity on the longitudinal and...
The model tested was a general research model of a swept-wing, jet-powered STOL transport with exter...
Four ejectors mounted in each pod under each wing and powered with compressed air were used to simul...
Effect of engine position and high lift devices on aerodynamic characteristics of external flow, jet...
An investigation of the longitudinal aerodynamic characteristics of an aspect ratio 4.735 airfoil ha...
Wind tunnel tests for V/STOL aircraft having direct-lift and lift-cruise jet nozzle
The low speed longitudinal characteristics of the jet flap STOL model were determined. The 17 percen...
Proximity effects of moving ground plane on aerodynamic characteristics of low speed transport aircr...
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...
A low speed investigation was conducted in the Langley V/STOL tunnel to determine the power-on stati...
Wind tunnel investigation of static longitudinal aerodynamic characteristics of semispan swept wing ...
Determination of low speed longitudinal aerodynamic characteristics of four engine externally blowin...
An investigation of the static longitudinal aerodynamic characteristics of a semispan STOL jet trans...
Wind tunnel investigation of jet transport airplane configuration with high thrust-weight ratio and ...
Ground effects investigation of STOL air-sea transport model with blowing over canard and wing flap
A wind-tunnel investigation has been made of the effects of ground proximity on the longitudinal and...
The model tested was a general research model of a swept-wing, jet-powered STOL transport with exter...
Four ejectors mounted in each pod under each wing and powered with compressed air were used to simul...
Effect of engine position and high lift devices on aerodynamic characteristics of external flow, jet...
An investigation of the longitudinal aerodynamic characteristics of an aspect ratio 4.735 airfoil ha...
Wind tunnel tests for V/STOL aircraft having direct-lift and lift-cruise jet nozzle