Active flow control system
作者： Claude G. Matalanis , Patrick Bowles , Brian E. Wake
DOI:
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摘要: An aircraft is provided and includes a fuselage including top tail, main rotor apparatus disposed at the of fuselage, which rotates one or more rotors to generate lift, an active flow control (AFC) system. The AFC system plasma actuators configured location adjacent and/or tail fuselage.
lens.org 参考文章(23)
Thomas C. Corke, Richard Spivey, Methods and apparatus for reducing drag via a plasma actuator ,(2007)
Mark Winfield Scott, Compact co-axial rotor system for a rotary wing aircraft and a control system therefor ,(2004)
Thomas C. Corke, Tommie L. Wood, Martiqua Post, Plasma actuators for drag reduction on wings, nacelles and/or fuselage of vertical take-off and landing aircraft ,(2006)
Thomas G. Tillman, Brian E. Wake, Streamlined bodies with counter-flow fluid injection ,(2000)
Wouter Haans, Jacob Johannes Nies, System And Method Of Operating An Active Flow Control System To Manipulate A Boundary Layer Across A Rotor Blade Of A Wind Turbine ,(2010)
Wesley K. Lord, Peter F. Lorber, Centrifugal air flow control ,(2000)
Seyed Gholamali Saddoughi, Method and apparatus for modulating flow separation ,(2003)
Subrata Roy, Devices Employing One or More Plasma Actuators ,(2015)
Sergey Macheret, Paul D. McClure, Dennis B. Finley, Plasma actuated vortex generators ,(2011)