Add to ORKGA wind-tunnel investigation was conducted to examine the low-speed static stability and control char...
Longitudinal and lateral stability data were obtained with the model out of and in ground effect ove...
A 1/8 scale jet-effects model was tested in the NASA Ames 11 ft transonic tunnel at static condition...
Results from the initial wind-tunnel test of a large-scale, highly maneuverable supersonic V/STOL fi...
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...
Four ejectors mounted in each pod under each wing and powered with compressed air were used to simul...
The stability and control characteristics of a four-engine turbofan STOL transport model having an e...
A wind-tunnel investigation has been made of the effects of ground proximity on the longitudinal and...
Full scale wind tunnel investigation of VTOL AIRCRAFT with jet ejector system for lift augmentatio
The aerodynamic characteristics of a six-engine (four lift, two lift-cruise) lift-engine model obtai...
Wind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stabilit
A wind-tunnel investigation was conducted with a vectored-thrust V/STOL fighter configuration. The m...
A wind tunnel test was conducted to obtain power on low speed characteristics of a twin fan vectored...
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel and in a scaled version of th...
Determination of low speed longitudinal aerodynamic characteristics of four engine externally blowin...
A wind-tunnel investigation was conducted to examine the low-speed static stability and control char...
Longitudinal and lateral stability data were obtained with the model out of and in ground effect ove...
A 1/8 scale jet-effects model was tested in the NASA Ames 11 ft transonic tunnel at static condition...
Results from the initial wind-tunnel test of a large-scale, highly maneuverable supersonic V/STOL fi...
Wind tunnel tests of static longitudinal and lateral characteristics of short takeoff aircraft with ...
Four ejectors mounted in each pod under each wing and powered with compressed air were used to simul...
The stability and control characteristics of a four-engine turbofan STOL transport model having an e...
A wind-tunnel investigation has been made of the effects of ground proximity on the longitudinal and...
Full scale wind tunnel investigation of VTOL AIRCRAFT with jet ejector system for lift augmentatio
The aerodynamic characteristics of a six-engine (four lift, two lift-cruise) lift-engine model obtai...
Wind tunnel tests of a VTOL jet fighter to determine aerodynamic characteristics including stabilit
A wind-tunnel investigation was conducted with a vectored-thrust V/STOL fighter configuration. The m...
A wind tunnel test was conducted to obtain power on low speed characteristics of a twin fan vectored...
A wind-tunnel investigation was conducted in the Langley V/STOL tunnel and in a scaled version of th...
Determination of low speed longitudinal aerodynamic characteristics of four engine externally blowin...
A wind-tunnel investigation was conducted to examine the low-speed static stability and control char...
Longitudinal and lateral stability data were obtained with the model out of and in ground effect ove...
A 1/8 scale jet-effects model was tested in the NASA Ames 11 ft transonic tunnel at static condition...