When a jet STOVL aircraft is in STOL operation the jets impinge on the ground and generate wall jets flowing radially outward from the points at which the jets impinge. When the forward flowing part of a wall jet meets the free stream flow it is rolled back on itself forming a parabolic shaped ground vortex. Positive pressures are induced on the lower surface of the configuration ahead of the ground vortex and suction pressures are induced over the ground vortex itself. In addition, the suction pressures induced aft of the jet out of ground effect are reduced and lifting pressures are induced on the upper surface. This study analyzes available pressure and force data and develops a method for estimating the forces and moments induced in gro...
The ground effects associated with V/STOL operation were examined and an effort was made to develop ...
The flow fields encountered by jet- and fan-powered Vertical/Short Takeoff and Landing (V/STOL) airc...
The data obtained during an investigation of the effects of the ground vortex on a generic wing-body...
The jet-induced forces generated on short takeoff and vertical landing (STOVL) aircraft when in clos...
When a jet STOVL aircraft is hovering, or in a crossflow, while close to the ground wall jets flowin...
The interaction of the free stream velocity on the wall jet formed by the impingement of deflected e...
Currently available methods for estimating the net suckdown induced on jet V/STOL aircraft hovering ...
Prediction techniques for jet induced lift effects during hover are available, relatively easy to us...
An experimental investigation was carried out to study the aerodynamics of an airfoil with a rectang...
The suckdown condition encountered when jet propelled, Vertical/Short Takeoff and Landing aircraft h...
Flow characteristics of impinging jets emanating from rectangular exit area converging nozzles of ex...
Flow field investigations were conducted at the NASA Ames-Dryden Flow Visualization Facility (water ...
NASA Ames is conducting a program to develop improved methods for predicting suckdown and hot-gas in...
The data obtained during an investigation of the effects of crossflow on the suckdown and fountain e...
The ability of the potential flow analysis (POTFAN) to predict the influence of ground proximity on ...
The ground effects associated with V/STOL operation were examined and an effort was made to develop ...
The flow fields encountered by jet- and fan-powered Vertical/Short Takeoff and Landing (V/STOL) airc...
The data obtained during an investigation of the effects of the ground vortex on a generic wing-body...
The jet-induced forces generated on short takeoff and vertical landing (STOVL) aircraft when in clos...
When a jet STOVL aircraft is hovering, or in a crossflow, while close to the ground wall jets flowin...
The interaction of the free stream velocity on the wall jet formed by the impingement of deflected e...
Currently available methods for estimating the net suckdown induced on jet V/STOL aircraft hovering ...
Prediction techniques for jet induced lift effects during hover are available, relatively easy to us...
An experimental investigation was carried out to study the aerodynamics of an airfoil with a rectang...
The suckdown condition encountered when jet propelled, Vertical/Short Takeoff and Landing aircraft h...
Flow characteristics of impinging jets emanating from rectangular exit area converging nozzles of ex...
Flow field investigations were conducted at the NASA Ames-Dryden Flow Visualization Facility (water ...
NASA Ames is conducting a program to develop improved methods for predicting suckdown and hot-gas in...
The data obtained during an investigation of the effects of crossflow on the suckdown and fountain e...
The ability of the potential flow analysis (POTFAN) to predict the influence of ground proximity on ...
The ground effects associated with V/STOL operation were examined and an effort was made to develop ...
The flow fields encountered by jet- and fan-powered Vertical/Short Takeoff and Landing (V/STOL) airc...
The data obtained during an investigation of the effects of the ground vortex on a generic wing-body...