Keyphrases
Aerodynamic Analysis
17%
Aerodynamic Characteristics
17%
Aerodynamic Damping
71%
Aerodynamic Performance
53%
Aerodynamic Performance Prediction
7%
Aeroelastic Analysis
17%
Aeroelastic Characteristics
71%
Aeroelastic Performance
17%
Aluminum Alloy Material
7%
Amplitude Magnification
53%
Artificial Neural Network Modeling
71%
Axial Compressor Rotor
71%
Backward Sweep
17%
Blade Aerodynamics
17%
Blade Curvature
71%
Blade Tip
17%
Blade Twist
53%
Compressor Rotor
14%
Curvature Constraint
71%
Deformation Process
17%
Electrical Contact Resistance
71%
Error Coefficient
23%
Exit Routes
17%
Flow Angle
17%
Flutter
17%
Forced Response
53%
Forward Lean
35%
Free-form Deformation
17%
Free-form Deformation Method
7%
Frequency Mistuning
35%
Gaussian Process
17%
Generator Optimization
23%
In-house Code
17%
Interfacial Materials
71%
Isentropic Efficiency
35%
Kriging
17%
Linear Correlation
17%
Low Speed Axial Compressor
71%
Low TCR
23%
Mistuning
71%
Multidisciplinary Design Optimization
17%
Numerical Methodology
71%
Numerical Optimization
71%
Optimization Approach
17%
Optimization Framework
17%
Peak Efficiency
17%
Polynomial Chaos Kriging
7%
Pressure Surface
17%
Process-based
17%
Response Mean
17%
Rotor
17%
Rotor Blade
17%
Self-organizing Map Method
7%
Streamwise
14%
Strength Requirement
7%
Structural Strength
7%
Thermal Grease
47%
Total Pressure Ratio
35%
Twist Angle
17%
Verification Analysis
7%
Vibration Amplitude
17%
Von Mises Stress
35%
Yield Limit
7%
Engineering
Aerodynamic Analysis
17%
Aerodynamic Damping
71%
Aerodynamic Performance
92%
Axial Compressors
71%
Backward Twist
17%
Blade Tip
17%
Compressor Rotor
100%
Computational Cost
14%
Computational Fluid Dynamics
14%
Design Method
71%
Design Optimization
14%
Design Space
14%
Dominant Component
10%
Engineering
14%
Exit Flow
17%
Finite Element Method
42%
Force Response
53%
Freeform Deformation
32%
Gaussians
17%
Isentropic Efficiency
50%
Maximum Stress
71%
Multidisciplinary Design Optimization
42%
Optimization Approach
17%
Optimization Method
42%
Peak Efficiency
17%
Penalty Function
14%
Performance Prediction
14%
Pressure Ratio
35%
Pressure Surface
17%
Rotor Blade
17%
Rotors
89%
Self-Organizing Map
14%
Streamwise
28%
Strength Requirement
14%
Structural Performance
14%
Structural Strength
14%
Surrogate Model
28%
T Cell Receptor
71%
Twist Angle
17%