simulation of plasma actuator on arbitrarily shaped surface ben mertz center for flow physics and...
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Simulation of Plasma Actuator on Arbitrarily Shaped Surface
Ben Mertz
Center for Flow Physics and Control
University of Notre Dame, Notre Dame, IN
Graduate Student Conference, August 27th, 2007
Outline
Background/Motivation Virtual Wing Shaping Plasma Actuators Lumped Circuit Model Generalized Coordinates
Flat Plate Test Case Future Work/Conclusions
Graduate Student Conference, August 27th, 2007
Benefits of LE+TE Control
-$410K on $30M airplane
- 2.6% part-card count
- 3.3% empty weight
- 1.3 % manufacturing cost
- 3.3% drag reduction
“Virtual Wing”
Motivation: Virtual Wing Shaping
Graduate Student Conference, August 27th, 2007
Airfoils Being Studied
Graduate Student Conference, August 27th, 2007
NLF213 (Voikov)
Optimized Airfoil (Shiokawa, et al.)
MO6-13-128 (Selig, et al.)
Actuator locationActuator location
Possible actuator location
Plasma Actuators
The plasma actuator in action appears as a diffuse plasma formed on the surface of the dielectric
exposed electrode insulation
AC voltage source
insulated electrode
substrate
The plasma actuator is an asymmetric arrangement of electrodes, one of which is insulated, on an aerodynamic surface.
Graduate Student Conference, August 27th, 2007
Lumped Circuit Model
Graduate Student Conference, August 27th, 2007
Orlov (2006)
Models plasma on a.c. time scale Values of Capacitors and Resistors depend on physical
constants and geometry of actuator
Computational Domain
Graduate Student Conference, August 27th, 2007
Orlov (2006)
Generalized Coordinates
Graduate Student Conference, August 27th, 2007
y
x
η
ζ
Plasma Extent
Graduate Student Conference, August 27th, 2007
Plasma Current
Graduate Student Conference, August 27th, 2007
Future Research
Graduate Student Conference, August 27th, 2007
Finish flat plate test case comparison Use code to simulate actuator on curved surface Perform flow simulations using body force results
for flat plate and curved surface cases Apply code to different airfoil shapes and evaluate
feasibility for flow control purposes using CFD simulations of airfoil shapes
Questions?
Graduate Student Conference, August 27th, 2007
Acknowledgements
A special thanks to …
Dr. Thomas Corke (advisor) and Dr. Dmitri Orlov
Orbital Research Inc.
Graduate Student Conference, August 27th, 2007