The ground effects associated with V/STOL operation were examined and an effort was made to develop the equipment and testing techniques needed for that understanding. Primary emphasis was on future experimental programs in the 40 x 80 and the 80 x 120 foot test sections and in the outdoor static test stand associated with these facilities. The commonly used experimental techniques are reviewed and data obtained by various techniques are compared with each other and with available estimating methods. These reviews and comparisons provide insight into the limitations of past studies and the testing techniques used and identify areas where additional work is needed. The understanding of the flow mechanics involved in hovering and in transitio...
Theoretical studies are made of three dimensional turbulent boundary layer behavior on fixed grounds...
The flow field measured around a hovering 70 percent scale vertical takeoff and landing (V/STOL) air...
Propulsion device-induced effects on V/STOL aircraft aerodynamics in hover and transition fligh
The flow fields encountered by jet- and fan-powered Vertical/Short Takeoff and Landing (V/STOL) airc...
A flow visualization study of several configurations of a jet-powered vertical takeoff and landing (...
The jet-induced forces generated on short takeoff and vertical landing (STOVL) aircraft when in clos...
The suckdown condition encountered when jet propelled, Vertical/Short Takeoff and Landing aircraft h...
Wind tunnel tests on a finite, knee-blowing-flapped wing and on a direct jet lift configuration were...
As part of a program to improve the methods for predicting the suckdown and hot gas ingestion for je...
Propulsion induced effects encountered by moderate- to high-disk loading STOVL or VSTOL aircraft out...
Available prediction methods applied to problems of aero/propulsion interactions for short takeoff a...
A moving-model ground-effect testing method was used to study the influence of rate-of-descent on th...
When a jet STOVL aircraft is in STOL operation the jets impinge on the ground and generate wall jets...
A ground-based testing technique is under development for the measurement of dynamic or time-depende...
The data obtained during an investigation of the effects of crossflow on the suckdown and fountain e...
Theoretical studies are made of three dimensional turbulent boundary layer behavior on fixed grounds...
The flow field measured around a hovering 70 percent scale vertical takeoff and landing (V/STOL) air...
Propulsion device-induced effects on V/STOL aircraft aerodynamics in hover and transition fligh
The flow fields encountered by jet- and fan-powered Vertical/Short Takeoff and Landing (V/STOL) airc...
A flow visualization study of several configurations of a jet-powered vertical takeoff and landing (...
The jet-induced forces generated on short takeoff and vertical landing (STOVL) aircraft when in clos...
The suckdown condition encountered when jet propelled, Vertical/Short Takeoff and Landing aircraft h...
Wind tunnel tests on a finite, knee-blowing-flapped wing and on a direct jet lift configuration were...
As part of a program to improve the methods for predicting the suckdown and hot gas ingestion for je...
Propulsion induced effects encountered by moderate- to high-disk loading STOVL or VSTOL aircraft out...
Available prediction methods applied to problems of aero/propulsion interactions for short takeoff a...
A moving-model ground-effect testing method was used to study the influence of rate-of-descent on th...
When a jet STOVL aircraft is in STOL operation the jets impinge on the ground and generate wall jets...
A ground-based testing technique is under development for the measurement of dynamic or time-depende...
The data obtained during an investigation of the effects of crossflow on the suckdown and fountain e...
Theoretical studies are made of three dimensional turbulent boundary layer behavior on fixed grounds...
The flow field measured around a hovering 70 percent scale vertical takeoff and landing (V/STOL) air...
Propulsion device-induced effects on V/STOL aircraft aerodynamics in hover and transition fligh