Keyphrases
Axial Flow Turbine
90%
Squealer Tip
62%
Squealer
59%
Flow Structure
53%
Aero-thermal
52%
Turbine Blade
51%
Tip Leakage Flow
48%
Axial Turbine
42%
Aerodynamic Loss
41%
Flow Characteristics
39%
Blade Tip
38%
Free Surface
38%
Torpedo-like Geometry
38%
HP Turbine
37%
Reynolds number
32%
Tip Gap
30%
Heat Transfer
27%
Turbine Stage
26%
Water Flow
24%
Relative Motion
23%
Aerodynamic Performance
22%
Carving
22%
Aerodynamic Field
22%
Genetic Algorithm
21%
Three-dimensional Viscous Flow
21%
Pressure Side
21%
Leakage Flow
20%
Twin Jets
19%
Jet Flow
19%
Fully Developed
19%
Open-cell Metal Foam
19%
Casing Groove
19%
Aerodynamic Characters
19%
Ground Traffic
19%
Viscous Flow Simulation
19%
Cavitation Performance
19%
Traffic Control
19%
Centrifugal Pump
19%
Radar Antennas
19%
Airport
19%
Parametric Approach
19%
Aerodynamics
19%
Free Surface Effect
18%
Suction Side
17%
Tip Flow
17%
Tip Vortex
17%
Tip Geometry
17%
Linear Turbine Cascade
16%
Particle Image Velocimetry
15%
Tip Loss
15%
Engineering
Axial Flow
100%
Flow Turbine
95%
Blade Tip
64%
Flow Structure
61%
Leakage Flow
59%
Blade Turbine
52%
Flow Characteristics
46%
Vortex
40%
Free Surface
38%
Experimental Investigation
35%
Suction Side
34%
Computational Fluid Dynamics
32%
Viscous Flow
32%
Reynolds' Number
30%
Metal Foam
28%
Relative Motion
25%
Pressure Side
24%
Genetic Algorithm
21%
Vortex Shedding
21%
Aerodynamic Performance
21%
Particle Image Velocimetry
21%
Flow Simulation
21%
Streamwise
20%
Centrifugal Pump
19%
Radar Antenna
19%
Traffic Control
19%
Free Surface Effect
18%
Heat Flux
17%
Navier-Stokes Equation
16%
Numerical Calculation
16%
Antenna
16%
High-Pressure Turbine
15%
Secondary Flow
15%
Flow Direction
14%
Nusselt Number
14%
Equation Turbulence Model
14%
Reynolds-Averaged Navier-Stokes
13%
Casing Treatment
13%
Aluminum Cell
12%
Parametric Study
12%
Aerodynamic Drag
12%
Aerothermal Performance
12%
Numerical Prediction
12%
Optimization Method
12%
Angle-of-Attack
12%
Gas Turbine
11%
Vorticity
11%
Reynolds Stress
10%
Pump Characteristic
10%
Two Dimensional
10%