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Characterization of DBD Plasma Actuators Performance without External Flow : Thrust-Voltage Quadratic Relationship in Logarithmic Space for Sinusoidal Excitation - Part IWe present results of thrust measurements of Dielectric Barrier Discharge (DBD) plasma actuators. We have used a test setup, measurement, and data processing methodology that we developed in prior work. The tests were conducted with High Density Polyethylene (HDPE) actuators of three thicknesses. The applied voltage driving the actuators was a pure sinusoidal waveform. The test setup was suspended actuators with a partial liquid interface. The tests were conducted at low ambient humidity. The thrust was measured with an analytical balance and the results were corrected for anti-thrust to isolate the plasma generated thrust. Applying this approach resulted in smooth and repeatable data. It also enabled curve fitting that yielded quadratic relations between the plasma thrust and voltage in log-log space at constant frequencies. The results contrast power law relationships developed in literature that appear to be a rough approximation over a limited voltage range.
Document ID
20170001288
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Ashpis, David E.
(NASA Glenn Research Center Cleveland, OH United States)
Laun, Matthew C.
(HX5 Sierra, LLC Cleveland, OH, United States)
Date Acquired
February 3, 2017
Publication Date
June 13, 2016
Subject Category
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN32757
Report Number: GRC-E-DAA-TN32757
Meeting Information
Meeting: AIAA Aviation 2016
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 081876.02.03.05.02.02
CONTRACT_GRANT: NNC15BA02B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Dielectric Barrier Discharge
Plasma Actuator
Flow Control
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