Electric Circuit Model for Aerodynamic Plasma Actuator
By D. Orlov, Thomas C. Corke, Mehul P. Patel. 2006
143 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Computational Mechanics
View Paper: https://www.semanticscholar.org/paper/8dcd509c783de31b50d05b55fbd6e8daedbf0505
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In Aerospace Engineering
In Computational Mechanics
Citations in the corpus
- Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control (2009, methodology): “In addition, lumped element actuator simulations reported in [25] suggest that using a dielectric material of lower dielectric constant can significantly increase the maximum achievable voltage before onset of saturation.”
- Single dielectric barrier discharge plasma enhanced aerodynamics: physics, modeling and applications (2009, methodology): “[109, 108] utilized the electrostatic model with the exponential weighting described by Orlov[78, 77] to compute the plasma body force using the Enloe et al.”
- Airflow control by non-thermal plasma actuators (2007, result): “Concerning the current pulses due to streamers, they are positive during the positive voltage half-period and negative during the negative one, contrary to recent results that show negative and positive pulses simultaneously [72, 73].”