Amanote Research
Register
Sign In
Flying Wing Flow Separation Control by Microsecond Pulsed Dielectric Barrier Discharge at High Reynolds Number
AIP Advances
- United States
doi 10.1063/1.5125847
Full Text
Open PDF
Abstract
Available in
full text
Categories
Nanotechnology
Astronomy
Physics
Nanoscience
Date
December 1, 2019
Authors
Zhong-guo Niu
Jie Liu
Hua Liang
Li-ke Xie
Zhi Su
Publisher
AIP Publishing
Related search
Adaptive Flow Control of Low Reynolds Number Aerodynamics Using a Dielectric Barrier Discharge Actuator
High-Lift Airfoil Separation With Dielectric Barrier Discharge Plasma Actuation
AIAA Journal
Aerospace Engineering
Atmospheric-Pressure Dielectric Barrier Discharge Generation by a Full-Bridge Flying Capacitor Multilevel Inverter
Plasma Science and Technology
Condensed Matter Physics
Active Flow Separation Control on a High-Lift Wing-Body Configuration Part 2: The Pulsed Blowing Application
Optimization of Dielectric Barrier Discharge Plasma Actuators for Active Aerodynamic Flow Control
AIAA Journal
Aerospace Engineering
Numerical Investigation on the CH4/CO2 Nanosecond Pulsed Dielectric Barrier Discharge Plasma at Atmospheric Pressure
AIP Advances
Nanotechnology
Astronomy
Physics
Nanoscience
High-Reynolds-Number Flow Past a Pipe
Journal of Fluid Science and Technology
Transfer Processes
Fluid Flow
Mechanical Engineering
Surface Modification of Polyimide Film by Dielectric Barrier Discharge at Atmospheric Pressure
Plasma Science and Technology
Condensed Matter Physics
Mean Flow and Turbulence Measurements in the Near Field of a Fighter Aircraft Wing-Tip Vortex at High Reynolds Number and Transonic Flow Conditions
ESAIM: Proceedings