2008/11/27 by A R Hoskinson, Alan R. Hoskinson, N Hershkowitz +3 · 3 citations
Engineering · Mathematics · #Actuator #Aerospace engineering #Dielectric barrier discharge #Electrical engineering #Engineering #Gas Dynamics and Kinetic Theory #Materials science #Physics #Plasma #Plasma Diagnostics and Applications #Plasma actuator #Plasma and Flow Control in Aerodynamics
paper · doi:10.1088/0022-3727/41/24/245209
openalex publication_date 2008/11/27 · openalex created_date 2025/10/10 · openalex updated_date 2026/08/05
We present the results of our experimental measurements of how variations in the discharge geometry of surface-mounted dielectric barrier discharges (DBDs) affect the force transferred to atmospheric pressure air. Our studies include both single barrier plasma actuators (one electrode insulated) and double barrier plasma actuators (both electrodes insulated) operated in quiescent air. Stagnation probe measurements of the induced air flow and direct force measurements using an electronic balance show that, for both actuator types, parallel time-averaged forces increase as the high voltage electrode diameter decreases. For single barrier actuators, this increase is exponential rather than linear as previously reported in the literature. The data from the two measurement techniques are directly proportional to one another. When the variation of velocity and pressure on all sides of an actuator are considered, the techniques show quantitative agreement.