Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils
Patent
1997-06-05
1999-09-28
Weldon, Kevin
Aeronautics and astronautics
Aircraft sustentation
Sustaining airfoils
B64C 2106
Patent
active
059574135
ABSTRACT:
The present invention involves a system for altering the aerodynamic shape and/or fluid flow field about a solid body. The preferred embodiment comprises a synthetic jet actuator embedded in a solid body, with the jet orifice built into the body surface. The synthetic jet actuator generates a series of fluid vortices emanating from the orifice so as to entrain fluid external to the actuator chamber and form a synthetic jet stream. A recirculating flow region is formed along the solid body surface about the synthetic jet orifice. As a result the apparent aerodynamic shape of the body is altered. Consequently, if the solid body is placed in a fluid flow field, the entire fluid flow field is altered by the operation of the synthetic jet actuator.
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Glezer Ari
Smith Barton L.
Trautman Mark A.
Georgia Tech Research Corporation
Weldon Kevin
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