The effect of geometry variations in the design of external deflectors for use with over-the-wing (OTW) configurations was studied at model scale and subsonic jet velocities. Included in the variations were deflector size and angle as well as wing size and flap setting. A conical nozzle (5.2-cm diameter) mounted at 0.1 chord above and downstream of the wing leading edges was used. The data indicate that external deflectors provide satisfactory takeoff and approach aerodynamic performance and acoustic characteristics for OTW configurations. These characteristics together with expected good cruise aerodynamics, since external deflectors are storable, may provide optimum OTW design configurations
Acoustic data obtained from a model-scale study with 5:1 slot nozzles are analyzed and correlated in...
Wind-tunnel investigations of the acoustic characteristics of the externally blown jet flap (EBF) an...
The noise caused by the interaction of the jet exhaust and a wing was measured under static conditio...
Acoustic spectral data obtained from a model-scale study of several over the wing (OTW) configuratio...
Future STOL aircraft may utilize engine-over-the-wing installations in which the exhaust nozzles are...
The effects of nozzle geometry and wing size on the aerodynamic performance of several 5:1 aspect ra...
Jet flap interaction acoustic data obtained statically from a model-scale study of STOL-OTW configur...
The correspondence of far field acoustic trends with changes in the characteristics of the flow fiel...
The effects on acoustic characteristics of nozzle type and location on a wing for STOL engine over-t...
On the basis of static aero/acoustic data obtained at model scale, the effect of exhaust nozzle size...
Surface pressure distributions were obtained with model-scale STOL-OTW configurations using various ...
Noise tests were conducted with a nozzle exhausting over a small scale model of an externally blown ...
Small-model experiments were conducted of the engine-over-the-wing concept using a D-shaped nozzle i...
The acoustics of simple engine over-the-wing configurations, with complete and partially attached je...
The sensitivity of flap interaction noise to variations in engine-under-the-wing externally blown fl...
Acoustic data obtained from a model-scale study with 5:1 slot nozzles are analyzed and correlated in...
Wind-tunnel investigations of the acoustic characteristics of the externally blown jet flap (EBF) an...
The noise caused by the interaction of the jet exhaust and a wing was measured under static conditio...
Acoustic spectral data obtained from a model-scale study of several over the wing (OTW) configuratio...
Future STOL aircraft may utilize engine-over-the-wing installations in which the exhaust nozzles are...
The effects of nozzle geometry and wing size on the aerodynamic performance of several 5:1 aspect ra...
Jet flap interaction acoustic data obtained statically from a model-scale study of STOL-OTW configur...
The correspondence of far field acoustic trends with changes in the characteristics of the flow fiel...
The effects on acoustic characteristics of nozzle type and location on a wing for STOL engine over-t...
On the basis of static aero/acoustic data obtained at model scale, the effect of exhaust nozzle size...
Surface pressure distributions were obtained with model-scale STOL-OTW configurations using various ...
Noise tests were conducted with a nozzle exhausting over a small scale model of an externally blown ...
Small-model experiments were conducted of the engine-over-the-wing concept using a D-shaped nozzle i...
The acoustics of simple engine over-the-wing configurations, with complete and partially attached je...
The sensitivity of flap interaction noise to variations in engine-under-the-wing externally blown fl...
Acoustic data obtained from a model-scale study with 5:1 slot nozzles are analyzed and correlated in...
Wind-tunnel investigations of the acoustic characteristics of the externally blown jet flap (EBF) an...
The noise caused by the interaction of the jet exhaust and a wing was measured under static conditio...