Surface pressure distributions were obtained with model-scale STOL-OTW configurations using various nozzles designed to promote flow attachment to the wing/flap surface. The nozzle configurations included slot-types and both circular and slot nozzles with external flow deflectors. The wing aerodynamic loading caused by the jet-induced lift is presented in conventional terms of delta p/q as a function of chordwise surface distance in the nozzle centerline plane as well as outboard of the nozzle centerline. Nozzle roof/deflector angle, chordwise location of the nozzle, wing size, and flap deflection angle are included in the geometric variables affecting the wing loading.
Wing aerodynamic loading caused by jet-induced lift associated with STOL-OTW configurations
Atmospheric Flight Mech. Conf. ; 1979 ; Boulder, CO, United States
1979-01-01
Report
Keine Angabe
Englisch
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