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Keyphrases
Aeroderivative Gas Turbine
29%
Aerodynamic Performance
37%
Aerofoil
28%
Annular Cascade
27%
Axial Velocity
37%
Base Pressure
31%
Design Process
25%
Edge Diameter
28%
Empirical Prediction
40%
Exit Mach number
39%
Exit Route
41%
Flow Angle
44%
Flow Field
32%
Flow Field Measurement
31%
Gas Turbine Engine
57%
Highly Loaded Turbine
28%
Improved Correlation
28%
Incidence Loss
28%
Leading Edge Geometry
56%
Linear Blade Cascade
31%
Loss Correlation
28%
Loss Prediction
28%
Low Aspect Ratio
39%
Low Speed
29%
NARX Model
28%
New Correlation
24%
Nozzle
37%
Off-design
76%
Off-design Condition
46%
Off-design Performance
38%
Prediction Method
68%
Preliminary Design Phase
40%
Pressure Ratio
43%
Profile Loss
50%
Reynolds number
24%
Rotor
81%
Secondary Flow
53%
Secondary Losses
77%
Single-stage
43%
Trailing Edge
34%
Transonic
59%
Transonic Turbine
81%
Transonic Turbine Stage
37%
Turbine Airfoil
28%
Turbine Blade
56%
Turbine Cascade
56%
Turbine Nozzle
75%
Turbine Parts
37%
Turning Angle
38%
Velocity-density
28%
Engineering
Aerodynamic Performance
37%
Aerodynamics
50%
Airfoil
48%
Aspect Ratio
42%
Axial Velocity
37%
Base Pressure
35%
Blade Passage
18%
Blade Turbine
59%
Computational Fluid Dynamics
21%
Density Ratio
28%
Derivative Gas Turbine
29%
Design Condition
53%
Design Process
24%
Design Speed
20%
Design System
24%
Dimensional Flow
29%
Disc Turbine
18%
Engine Data
18%
Exit Flow
65%
Exit Mach Number
51%
Experimental Result
92%
Field Measurement
31%
Flow Condition
21%
Flow Distribution
87%
Flow Visualization
29%
Gas Turbine
29%
Gas Turbine Engine
56%
High-Pressure Turbine
28%
Leading Edge
85%
Low Aspect Ratio
49%
Mach Number
45%
Output Parameter
18%
Preliminary Analysis
28%
Preliminary Design
46%
Preliminary Design Phase
40%
Pressure Difference
18%
Pressure Distribution
32%
Pressure Flow
21%
Pressure Ratio
40%
Recurrent Neural Network
18%
Reynolds' Number
26%
Rotor Blade
23%
Rotors
100%
Scaling Factor
18%
Secondary Flow
59%
Single Output
20%
Static Pressure
21%
Test Arrangement
28%
Trailing Edge
43%
Turbines Airfoil
28%
