Engineering
Control Flow
100%
Dielectrics
94%
Boundary Layer
79%
Layer Interaction
76%
Airfoil
73%
Nanosecond
65%
Separation Control
61%
Actuation
52%
Reynolds' Number
44%
Laminar Separation Bubble
43%
Mixing Layer
42%
Shear Layer
38%
Oblique Shock
34%
Energy Engineering
33%
Turbulent Boundary Layer
32%
Cavity Flow
30%
Fluidics
29%
Particle Image Velocimetry
27%
Reduced Order Model
27%
Reattachment
27%
Flaps
25%
Proper Orthogonal Decomposition
24%
Angle-of-Attack
24%
Flow Field
24%
Schlieren
23%
Vortex
23%
Streamwise
23%
Feedback Control System
21%
Coherent Structure
20%
Separation Bubble
18%
Pulse Energy
18%
Sweep Angle
18%
Flow Physic
17%
Trailing Edge
16%
Leading Edge
16%
Direct Numerical Simulation
15%
Active Control
14%
Computer Simulation
14%
Flow Visualization
12%
Suction Side
12%
Boundary Layer Transition
12%
Control System
12%
Separated Region
11%
Flat Plate
11%
Aspect Ratio
11%
Boundary Layer Separation
11%
Control Input
11%
Pulse Amplitude
10%
Flow Structure
10%
Constant Temperature Anemometry
9%
Keyphrases
Dielectric Barrier Discharge Plasma Actuator
34%
Pulse Drive
25%
Nanosecond Pulse
25%
Separation Control
21%
High-lift Airfoil
18%
Flow Control
16%
Span-wise
16%
Dielectric Barrier Discharge Plasma
15%
Active Flow Control
15%
Plasma Actuation
13%
Near Stall
13%
Plunging Motion
13%
Turbulent Boundary Layers
13%
Volumetric Study
12%
Pulse Polarity
12%
Boundary Layer Interaction
12%
Pressure Film
12%
Hot-film
12%
Flap
12%
Laminar Separation Bubble
12%
Oblique Shock
12%
Shock Wave Boundary Layer Interaction
12%
Low-frequency Unsteadiness
11%
Actuator
11%
Airfoil
10%
Separation Bubble
10%
Compression Ramp
10%
Control Authority
9%
Mixing Layer
9%
Angle of Attack
9%
Proper Orthogonal Decomposition
9%
Control Actuator
8%
Flow Field
8%
Shock
8%
Numerical Simulation
8%
Boundary Layer
8%
Dielectric Barrier Discharge
8%
Post-stall
8%
Stochastic Estimation
8%
Velocity Field
8%
Thermal Perturbation
7%
Sweep Angle
7%
Particle Image Velocimetry
7%
Constant Temperature Anemometry
7%
DBD Plasma Actuator
7%
Sweeping
7%
Wing Section
7%
Dielectric Thickness
7%
Layer Condition
6%
Vortex-body Interaction
6%