发明名称 |
Dielectric barrier discharge flight control system through modulated boundary layer transition |
摘要 |
OF DISCLOSURE An aerodynamic control system incorporates multiple Dielectric Barrier Discharge (DBD) flow control actuators adjacent a surface of an airborne vehicle in a path of laminar boundary layer flow over the surface. A control computer receives a control input and selectively distributes power to an activation array selected from the DBD flow control actuators for transition to a first operating condition tripping the laminar boundary layer at selected streamwise locations for turbulent flow. When the control computer removes the distributed power the DBD flow control actuators return to a second operating condition restoring the laminar boundary layer. -14- 70a 70b 70c 18b 76 74b |
申请公布号 |
AU2013200785(A1) |
申请公布日期 |
2013.11.21 |
申请号 |
AU20130200785 |
申请日期 |
2013.02.08 |
申请人 |
THE BOEING COMPANY |
发明人 |
OSBORNE, BRADLEY A.;SCHWIMLEY, SCOTT L.;SILKEY, JOSEPH S. |
分类号 |
B64C13/50;B64C13/24 |
主分类号 |
B64C13/50 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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