Add to ORKGGround effects investigation of STOL air-sea transport model with blowing over canard and wing flap
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
The Langley 1/8-scale V/STOL model tunnel was used to qualitatively determine the flow fields associ...
A STOL fighter model employing the vectored-engine-over wing concept was tested at low speeds in the...
Determination of low speed longitudinal aerodynamic characteristics of four engine externally blowin...
Proximity effects of moving ground plane on aerodynamic characteristics of low speed transport aircr...
A generalized wind-tunnel model with canard and wing planforms typical of highly maneuverable aircra...
The model tested was a general research model of a swept-wing, jet-powered STOL transport with exter...
A propulsive wind/canard model was tested at STOL operating conditions in the NASA Langley Research ...
The canard had an exposed area of 28.0 percent of the wing reference area and was located in the cho...
A generalized wind-tunnel model, typical of highly maneuverable aircraft, was tested in the Langley ...
Wind tunnel tests on a finite, knee-blowing-flapped wing and on a direct jet lift configuration were...
An analysis of the relative influences of for-ward lift-enhancing surfaces on the overall lift and d...
An investigation of the longitudinal aerodynamic characteristics of an aspect ratio 4.735 airfoil ha...
A wind-tunnel investigation was made of the low-speed characteristics of a canard configuration havi...
The low speed longitudinal characteristics of the jet flap STOL model were determined. The 17 percen...
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
The Langley 1/8-scale V/STOL model tunnel was used to qualitatively determine the flow fields associ...
A STOL fighter model employing the vectored-engine-over wing concept was tested at low speeds in the...
Determination of low speed longitudinal aerodynamic characteristics of four engine externally blowin...
Proximity effects of moving ground plane on aerodynamic characteristics of low speed transport aircr...
A generalized wind-tunnel model with canard and wing planforms typical of highly maneuverable aircra...
The model tested was a general research model of a swept-wing, jet-powered STOL transport with exter...
A propulsive wind/canard model was tested at STOL operating conditions in the NASA Langley Research ...
The canard had an exposed area of 28.0 percent of the wing reference area and was located in the cho...
A generalized wind-tunnel model, typical of highly maneuverable aircraft, was tested in the Langley ...
Wind tunnel tests on a finite, knee-blowing-flapped wing and on a direct jet lift configuration were...
An analysis of the relative influences of for-ward lift-enhancing surfaces on the overall lift and d...
An investigation of the longitudinal aerodynamic characteristics of an aspect ratio 4.735 airfoil ha...
A wind-tunnel investigation was made of the low-speed characteristics of a canard configuration havi...
The low speed longitudinal characteristics of the jet flap STOL model were determined. The 17 percen...
An exploratory wind-tunnel investigation has been made to determine the lift effects of blowing from...
The Langley 1/8-scale V/STOL model tunnel was used to qualitatively determine the flow fields associ...
A STOL fighter model employing the vectored-engine-over wing concept was tested at low speeds in the...