Comparison of the Linear and Spanwise-Segmented DBD Plasma Actuators on Flow Control Around a NACA0015 Airfoil
Author:
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Subject
Condensed Matter Physics,Nuclear and High Energy Physics
Link
http://xplorestaging.ieee.org/ielx7/27/8097139/08053907.pdf?arnumber=8053907
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1. An experimental investigation on the flow control of the partially stepped NACA0012 airfoil at low Reynolds numbers;Ocean Engineering;2024-08
2. Flow and performance effects of a phenomenological model for a DBD actuator under different operating parameters;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2023-09-12
3. A novel LC‐based bipolar pulsed power supply for dielectric barrier discharge excimer lamps;International Journal of Circuit Theory and Applications;2023-04-22
4. Analysis and Design of a Compact Bipolar High-Voltage Short-Pulse Power Supply for DBD Application;IEEE Transactions on Plasma Science;2022-11
5. Vortical flow characteristics of a slender delta wing in ground effect;Ocean Engineering;2022-10
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