Dielectric Barrier Discharge Plasma Actuator Thrust Measurement Methodology Incorporating Antithrust Hypothesis [PDF]
The thrust of the dielectric barrier discharge plasma actuator is the plasma body force minus the wall shear force,and it equals the net induced momentum.
Ashpis, David E., Laun, Matthew C.
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Effect of Turbulence Modeling on an Excited Jet [PDF]
The flow dynamics in a high-speed jet are dominated by unsteady turbulent flow structures in the plume. Jet excitation seeks to control these flow structures through the natural instabilities present in the initial shear layer of the jet.
Brown, Clifford A., Hixon, Ray
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Deployable vortex generators for low Reynolds numbers applications powered by cephalopods inspired artificial muscles. [PDF]
Mamman R +6 more
europepmc +1 more source
Scalability of Localized Arc Filament Plasma Actuators [PDF]
Temporal flow control of a jet has been widely studied in the past to enhance jet mixing or reduce jet noise. Most of this research, however, has been done using small diameter low Reynolds number jets that often have little resemblance to the much ...
Brown, Clifford A.
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Synthetic jets as a flow control device for performance enhancement of vertical axis hydrokinetic turbines: A 3D computational study. [PDF]
Botero N +3 more
europepmc +1 more source
Dielectric Barrier Discharge (DBD) Plasma Actuators Thrust-Measurement Methodology Incorporating New Anti-Thrust Hypothesis [PDF]
We discuss thrust measurements of Dielectric Barrier Discharge (DBD) plasma actuators devices used for aerodynamic active flow control. After a review of our experience with conventional thrust measurement and significant non-repeatability of the results,
Ashpis, David E., Laun, Matthew C.
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Numerical Analysis of a Bidirectional Synthetic Jet for Active Flow Control [PDF]
Nishino, Takafumi, Savill, Mark A.
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Innovative Application of Cold Plasma Technology in Meat and Its Products. [PDF]
Jayasena DD +3 more
europepmc +1 more source
Combustion-Powered Actuation for Dynamic Stall Suppression - Simulations and Low-Mach Experiments [PDF]
An investigation on dynamic-stall suppression capabilities of combustion-powered actuation (COMPACT) applied to a tabbed VR-12 airfoil is presented. In the first section, results from computational fluid dynamics (CFD) simulations carried out at Mach ...
Bowles, Patrick O. +7 more
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Thrust Measurement of Dielectric Barrier Discharge (DBD) Plasma Actuators: New Anti-Thrust Hypothesis, Frequency Sweeps Methodology, Humidity and Enclosure Effects [PDF]
We discuss thrust measurements of Dielectric Barrier Discharge (DBD) plasma actuators devices used for aerodynamic active flow control. After a review of our experience with conventional thrust measurement and significant non-repeatability of the results,
Ashpis, David E., Laun, Matthew C.
core +1 more source

