Engineering
Aerodynamic Damping
20%
Aerodynamic Design
20%
Aerodynamic Performance
75%
Axial Compressors
20%
Axial Flow Fan
20%
Axial-Flow Compressors
20%
Backplate
20%
Bond Coat
20%
Centrifugal Compressor
20%
Chord Length
33%
Compressor Rotor
28%
Computational Fluid Dynamics
30%
Covariance Matrix
20%
Cracking Behavior
40%
Design Method
20%
Design Optimization
44%
Design Stage
20%
Diffusers
20%
Ducted Fan
27%
Exit Flow
25%
Finite Element Method
22%
Freeform Deformation
56%
Leakage Flow
25%
Maximum Stress
37%
Multidisciplinary Design Optimization
32%
Multiobjective Genetic Algorithm
25%
Multiobjective Optimization
27%
Optimization Approach
45%
Optimization Method
23%
Optimization Strategy
24%
Optimum Design
26%
Parametric Study
25%
Peak Efficiency
18%
Performance Improvement
20%
Pressure Fluctuation
20%
Pressure Loss Coefficient
20%
Pressure Ratio
48%
Robust Design
20%
Rotors
100%
Service Condition
20%
Shock Strength
20%
Singular Value Decomposition
20%
Steam Turbines
20%
Structural Constraint
40%
Surrogate Model
34%
Temperature Fluctuation
20%
Turbomachine Blades
30%
Uncertainty Quantification
19%
Wave Motion
20%
Winglets
20%
Keyphrases
Active Subspace
20%
Aerodynamic Damping
20%
Aerodynamic Performance
61%
Aeroelastic Characteristics
20%
Aerospace Design
20%
Airfoil Aerodynamics
20%
Axial Compressor
20%
Axial Compressor Rotor
20%
Axial Fan
20%
Axial Flow Fan
20%
Backing Plate
20%
Blade Curvature
61%
Blade Twist
28%
Bond Coat
20%
Canting Angle
20%
Clearance Effects
20%
Compressor Performance
25%
Compressor Stator
20%
Cracking Behavior
20%
Curvature Constraint
30%
Diffuser
27%
Ducted Fan
20%
Fan Rotor
74%
Fan Stage
20%
FE Analysis
20%
Forming Method
20%
Free-form Deformation
32%
Freeform
20%
Interface Asperity
40%
Low Speed Axial Compressor
20%
Mistuning
20%
Multidisciplinary Design Optimization
30%
Non-uniform Tip Clearance
20%
Numerical Methodology
20%
Numerical Optimization
20%
Oxide Thickness
32%
Performance Improvement
20%
Robust Optimization
40%
Static Stress
20%
Steam Turbine
20%
Structural Constraints
40%
Sweeping
33%
Thermally Grown Oxide
20%
Total Pressure Ratio
23%
Trailing Edge
22%
Transonic Centrifugal Compressor
20%
Turbocharger Compressor
20%
Turbofan
20%
Unsteady Shock Wave
20%
Winglet
20%
