Results 71 to 80 of about 3,987 (188)

Dielectric Barrier Discharge Plasma Actuator Thrust Measurement Methodology Incorporating Antithrust Hypothesis [PDF]

open access: yes
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.
core   +1 more source

Effect of Turbulence Modeling on an Excited Jet [PDF]

open access: yes
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
core   +1 more source

Deployable vortex generators for low Reynolds numbers applications powered by cephalopods inspired artificial muscles. [PDF]

open access: yesiScience, 2023
Mamman R   +6 more
europepmc   +1 more source

Scalability of Localized Arc Filament Plasma Actuators [PDF]

open access: yes
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.
core   +1 more source

Dielectric Barrier Discharge (DBD) Plasma Actuators Thrust-Measurement Methodology Incorporating New Anti-Thrust Hypothesis [PDF]

open access: yes
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

Innovative Application of Cold Plasma Technology in Meat and Its Products. [PDF]

open access: yesFood Sci Anim Resour, 2023
Jayasena DD   +3 more
europepmc   +1 more source

Combustion-Powered Actuation for Dynamic Stall Suppression - Simulations and Low-Mach Experiments [PDF]

open access: yes
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
core   +1 more source

Thrust Measurement of Dielectric Barrier Discharge (DBD) Plasma Actuators: New Anti-Thrust Hypothesis, Frequency Sweeps Methodology, Humidity and Enclosure Effects [PDF]

open access: yes
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

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