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Keyphrases
Aeroderivative Gas Turbine
31%
Aerodynamic Performance
40%
Aerofoil
30%
Annular Cascade
29%
Axial Velocity
40%
Base Pressure
33%
Design Process
27%
Edge Diameter
31%
Empirical Prediction
44%
Exit Mach number
43%
Exit Route
44%
Flow Angle
48%
Flow Field
35%
Flow Field Measurement
33%
Gas Turbine Engine
62%
Highly Loaded Turbine
30%
Improved Correlation
31%
Incidence Loss
30%
Leading Edge Geometry
61%
Linear Blade Cascade
33%
Loss Correlation
31%
Loss Prediction
30%
Low Aspect Ratio
43%
Low Speed
32%
NARX Model
30%
New Correlation
27%
Nozzle
41%
Off-design
82%
Off-design Condition
50%
Off-design Performance
41%
Prediction Method
74%
Preliminary Design Phase
44%
Pressure Ratio
47%
Profile Loss
55%
Reynolds number
27%
Rotor
88%
Secondary Flow
57%
Secondary Losses
83%
Single-stage
47%
Trailing Edge
37%
Transonic
64%
Transonic Turbine
88%
Transonic Turbine Stage
40%
Turbine Airfoil
30%
Turbine Blade
61%
Turbine Cascade
61%
Turbine Nozzle
81%
Turbine Parts
40%
Turning Angle
41%
Velocity-density
30%
Engineering
Aerodynamic Performance
40%
Aerodynamics
54%
Airfoil
52%
Aspect Ratio
45%
Axial Velocity
40%
Base Pressure
38%
Blade Passage
20%
Blade Turbine
64%
Density Ratio
30%
Derivative Gas Turbine
31%
Design Condition
58%
Design Process
27%
Design Speed
22%
Design System
27%
Dimensional Flow
32%
Disc Turbine
20%
Engine Data
20%
Exit Flow
71%
Exit Mach Number
56%
Experimental Result
100%
Field Measurement
33%
Flow Condition
23%
Flow Distribution
95%
Flow Visualization
32%
Gas Turbine
32%
Gas Turbine Engine
61%
High-Pressure Turbine
30%
Leading Edge
93%
Low Aspect Ratio
53%
Mach Number
49%
Output Parameter
20%
Preliminary Analysis
30%
Preliminary Design
50%
Preliminary Design Phase
44%
Pressure Difference
20%
Pressure Distribution
35%
Pressure Flow
23%
Pressure Ratio
44%
Recurrent Neural Network
20%
Reynolds' Number
28%
Rotor Blade
25%
Rotors
98%
Scaling Factor
20%
Secondary Flow
64%
Single Output
21%
Static Pressure
23%
Test Arrangement
30%
Test Result
20%
Trailing Edge
47%
Turbines Airfoil
30%
