Separation Flow Control of a Generic Ground Vehicle Using an SDBD Plasma Actuator
Quiescent flow and wind tunnel tests were performed to gain additional physical insights into flow control for automotive aerodynamics using surface dielectric barrier discharge plasma actuators. First, the aerodynamic characteristics of ionic wind were studied, and a maximum induced velocity of 3.3...
Main Authors: | Zheng Hui, Xingjun Hu, Peng Guo, Zewei Wang, Jingyu Wang |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2019-10-01
|
Series: | Energies |
Subjects: | |
Online Access: | https://www.mdpi.com/1996-1073/12/20/3805 |
Similar Items
-
The Effect of Single Dielectric Barrier Discharge Actuators in Reducing Drag on an Ahmed Body
by: Saber Karimi, et al.
Published: (2020-12-01) -
Aerodynamic Drag Analysis of Autonomous Electric Vehicle Platoons
by: Sai Teja Kaluva, et al.
Published: (2020-08-01) -
Stall Control by Plasma Actuators: Characterization along the Airfoil Span
by: Giulia Zoppini, et al.
Published: (2020-03-01) -
The Effect of Plasma Actuator Placement on Drag Coefficient Reduction of Ahmed Body as an Aerodynamic Model
by: James Julian, et al.
Published: (2016-02-01) -
Mechanisms of Control Authority by Nanosecond Pulsed Dielectric Barrier Discharge Actuators on Flow Separation
by: Christoforos Skourides, et al.
Published: (2019-07-01)