Engineering
Shear Layer
100%
Axisymmetric
75%
Boundary Layer
68%
Base Flow
57%
Layer Interaction
52%
Mixing Layer
50%
Particle Image Velocimetry
36%
Streamwise
35%
Reattachment
34%
Base Pressure
31%
Supersonic Flow
31%
Butterfly Valve
31%
Vortex
27%
Free Shear Layer
27%
Experimental Investigation
25%
Two Dimensional
23%
Scale Structure
23%
Mach Number
23%
Schlieren
23%
Control Flow
23%
Flow Field
20%
Centerline
20%
Flaps
19%
Compressibility
19%
Angle-of-Attack
17%
High Resolution
17%
Separated Flow
17%
Flow Separation
16%
Diffusers
15%
Flow Visualization
15%
Turbulent Boundary Layer
15%
Pressure Sensitive Paints
15%
Probability Density Function
15%
Pressure Recovery
15%
Compressible Flow
15%
Ejector
14%
Normal Shock Wave
13%
Reynolds Stress
13%
Pressure Distribution
12%
Flow Structure
12%
Oblique Shock
12%
Planar Laser-Induced Fluorescence
12%
Pressure Fluctuation
12%
Convection Velocity
11%
Operating Characteristic
11%
Rotational
11%
Stagnation Pressure
11%
Doppler Velocimeter
11%
Static Pressure
11%
Velocity Field
11%
Keyphrases
Flow Field
90%
Shear Layer
77%
Velocity Measurement
44%
Shock Wave Boundary Layer Interaction
39%
Mixing Layer
38%
Three-dimensional (3D)
36%
Baseflow
33%
Butterfly Valve
31%
Boundary Layer
30%
Free Stream
30%
Large-scale Structure
30%
Supersonic Base Flow
26%
Streamwise
26%
Base Pressure
26%
Near Wake
26%
Reattachment
25%
Free Shear Layers
25%
Compressible Mixing Layer
24%
Normal Shock
23%
Flap
23%
Supersonic Flow
23%
Pressure Measurement
22%
Turbulent Structure
21%
Mach number
21%
Shock
20%
Particle Image Velocimetry
19%
Bleeding
18%
Valve Disc
17%
Two Dimensional
17%
Separated Flows
17%
Entrainment
16%
Axisymmetric Jet
16%
Ends-in-view
16%
Compressibility
16%
Angle of Attack
16%
Mean Velocity
15%
Interaction Control
15%
High-resolution
15%
Span-wise
15%
Mie Scattering
14%
Near-field
14%
Pressure Sensitive Paint
14%
Recirculation Region
14%
Laser Doppler Velocimetry
14%
Recompression
14%
Diffuser
13%
Plasma Actuator
13%
Aeroelasticity
13%
Compressible Flow
13%
Normal Shock Wave
13%