Dynamic Stall Control around Practical Airfoil Using Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators

Dynamic Stall Control around Practical Airfoil Using Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators

The flow control effects of a nanosecond-pulse-driven dielectric barrier discharge plasma actuator (ns-DBDPA) in dynamic stall flow were experimentally investigated. The ns-DBDPA was installed on the leading edge of an airfoil model designed in the form of a helicopter blade. The model was oscillate...

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Bibliographic Details
Main Authors: Yuto Iwasaki, Taku Nonomura, Koki Nankai, Keisuke Asai, Shoki Kanno, Kento Suzuki, Atsushi Komuro, Akira Ando, Keisuke Takashima, Toshiro Kaneko, Hidemasa Yasuda, Kenji Hayama, Tomoka Tsujiuchi, Tsutomu Nakajima, Kazuyuki Nakakita
Format: Article
Language:English
Published: MDPI AG 2020-03-01
Series:Energies
Subjects:
flow control
dynamic stall
plasma actuators
nanosecond pulse discharge
pressure measurement
Online Access:https://www.mdpi.com/1996-1073/13/6/1376

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https://www.mdpi.com/1996-1073/13/6/1376

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