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Numerical Simulation of a High-Lift Configuration with Embedded Fluidic ActuatorsNumerical simulations have been performed for a vertical tail configuration with deflected rudder. The suction surface of the main element of this configuration is embedded with an array of 32 fluidic actuators that produce oscillating sweeping jets. Such oscillating jets have been found to be very effective for flow control applications in the past. In the current paper, a high-fidelity computational fluid dynamics (CFD) code known as the PowerFLOW(Registered TradeMark) code is used to simulate the entire flow field associated with this configuration, including the flow inside the actuators. The computed results for the surface pressure and integrated forces compare favorably with measured data. In addition, numerical solutions predict the correct trends in forces with active flow control compared to the no control case. Effect of varying yaw and rudder deflection angles are also presented. In addition, computations have been performed at a higher Reynolds number to assess the performance of fluidic actuators at flight conditions.
Document ID
20150000541
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Vatsa, Veer N.
(NASA Langley Research Center Hampton, VA, United States)
Casalino, Damiano
(Exa GmbH Stutgart, Germany)
Lin, John C.
(NASA Langley Research Center Hampton, VA, United States)
Appelbaum, Jason
(Exa GmbH Stutgart, Germany)
Date Acquired
January 16, 2015
Publication Date
June 16, 2014
Subject Category
Fluid Mechanics And Thermodynamics
Aircraft Design, Testing And Performance
Aerodynamics
Report/Patent Number
NF1676L-17600
Meeting Information
Meeting: (AVIATION 2014) AIAA Aviation and Aeronautics Forum and Exposition
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 475122.02.07.03.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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