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Characterization of DBD Plasma Actuators Performance Without External Flow - Part I: Thrust-Voltage Quadratic Relationship in Logarithmic Space for Sinusoidal ExcitationResults of characterization of Dielectric Barrier Discharge (DBD) plasma actuators without external flow are presented. The results include aerodynamic and electric performance of the actuators without external flow for different geometrical parameters, dielectric materials and applied voltage level and wave form.
Document ID
20170004724
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Ashpis, David E.
(NASA Glenn Research Center Cleveland, OH United States)
Laun, Matthew C.
(HX5 Sierra, LLC Cleveland, OH, United States)
Date Acquired
May 25, 2017
Publication Date
June 15, 2016
Subject Category
Aeronautics (General)
Numerical Analysis
Plasma Physics
Report/Patent Number
AIAA-2016-4013
GRC-E-DAA-TN33066
Report Number: AIAA-2016-4013
Report Number: GRC-E-DAA-TN33066
Meeting Information
Meeting: AIAA Aviation-Plasma dynamics and Lasers Conference 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
Flow Control
Plasma Actuator
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