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Engineering
Experimental Result
100%
Rotors
98%
Flow Distribution
95%
Leading Edge
93%
Exit Flow
71%
Blade Turbine
64%
Secondary Flow
64%
Gas Turbine Engine
61%
Design Condition
58%
Exit Mach Number
56%
Aerodynamics
54%
Low Aspect Ratio
53%
Preliminary Design
50%
Airfoil
49%
Mach Number
49%
Aspect Ratio
45%
Preliminary Design Phase
44%
Aerodynamic Performance
40%
Axial Velocity
40%
Trailing Edge
38%
Base Pressure
38%
Pressure Ratio
37%
Pressure Distribution
35%
Field Measurement
33%
Flow Visualization
32%
Dimensional Flow
32%
Gas Turbine
32%
Derivative Gas Turbine
31%
Test Arrangement
30%
Turbines Airfoil
30%
High-Pressure Turbine
30%
Density Ratio
30%
Preliminary Analysis
30%
Reynolds' Number
28%
Design System
27%
Design Process
27%
Rotor Blade
25%
Static Pressure
23%
Pressure Flow
23%
Computational Fluid Dynamics
23%
Flow Condition
23%
Single Output
21%
Recurrent Neural Network
20%
Engine Data
20%
Disc Turbine
20%
Output Parameter
20%
Scaling Factor
20%
Pressure Difference
20%
Blade Passage
20%
Test Result
20%
Keyphrases
Rotor
67%
Turbine Nozzle
61%
Transonic Turbine
59%
Off-design
53%
Leading Edge Geometry
47%
Transonic
46%
Secondary Losses
45%
Prediction Method
40%
Turbine Cascade
40%
Profile Loss
38%
Preliminary Design Phase
36%
Off-design Condition
35%
Linear Blade Cascade
33%
Gas Turbine Engine
32%
Turbine Blade
30%
Transonic Turbine Stage
30%
Loss Prediction
30%
Velocity-density
30%
Flow Field Measurement
30%
Improved Correlation
29%
Single-stage
28%
Secondary Flow
27%
Exit Mach number
26%
New Correlation
25%
Low Aspect Ratio
24%
Turning Angle
24%
Exit Route
24%
Base Pressure
23%
Turbine Rotor
23%
Design Process
22%
Nozzle
22%
Pressure Ratio
22%
Tip Clearance
22%
Flow Field
21%
Empirical Prediction
20%
Axial Velocity
20%
Turbine Parts
20%
Aerodynamic Performance
20%
Aeroderivative Gas Turbine
20%
Incidence Loss
20%
Turbine Airfoil
20%
Aerofoil
20%
Turbine Shroud
20%
Static Pressure
20%
Edge Diameter
18%
Loss Correlation
18%
Rig Test
17%
Flow Angle
17%
Trailing Edge
17%
Vane
17%
