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A Mach 4 wind tunnel for plasma / boundary layer interaction studies
Bradley DeBlauw
,
Craig Dutton
,
Gregory Elliott
Aerospace Engineering
Mechanical Science and Engineering
Materials Research Laboratory
Research output
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Keyphrases
Fluid Dynamics
100%
Wind Tunnel
100%
Dynamic Mechanism
100%
Interaction Studies
100%
Boundary Layer Interaction
100%
Plasma Boundary
100%
Flow Field
50%
Measurement Techniques
50%
Computational Modeling
50%
Boundary Layer
50%
Actuator
50%
Discharge Time
50%
Dynamic Interaction
50%
Schlieren Imaging
50%
Pressure Distribution
50%
Pressure Measurement
50%
Modeling Effort
50%
Vortical Structures
50%
Plasma Actuator
50%
Arc Discharge
50%
Laser-induced Optical Breakdown
50%
Supersonic Boundary Layer
50%
Radio-frequency Discharge
50%
Downstream Pressure
50%
Pulsed Plasma
50%
Engineering
Boundary Layer
100%
Layer Interaction
100%
Tunnel
100%
Fluid Dynamics
50%
Actuator
50%
Experimental Result
25%
Radio Frequency
25%
Schlieren
25%
Downstream Pressure
25%
Primary Fluid
25%
Pressure Distribution
25%
Flow Distribution
25%
Physics
Wind Tunnels
100%
Boundary Layer Plasmas
100%
Blood Plasma
100%
Actuator
33%
Fluid Dynamics
33%
Computational Modeling
16%
Pressure Measurement
16%
Flow Distribution
16%
Pressure Distribution
16%
Boundary Layer
16%
Arc Discharge
16%
Radio Frequency Discharge
16%
Supersonic Boundary Layer
16%