Engineering
Rotors
100%
Aerodynamic Performance
96%
Pressure Ratio
70%
Design Optimization
65%
Freeform Deformation
56%
Surrogate Model
54%
Chord Length
54%
Multidisciplinary Design Optimization
52%
Turbomachine Blades
50%
Ducted Fan
47%
Multiobjective Optimization
47%
Optimum Design
46%
Optimization Approach
45%
Leakage Flow
45%
Exit Flow
45%
Multiobjective Genetic Algorithm
45%
Optimization Strategy
44%
Finite Element Method
42%
Pressure Loss Coefficient
40%
Shock Strength
40%
Structural Constraint
40%
Diffusers
40%
Covariance Matrix
40%
Singular Value Decomposition
40%
Design Stage
40%
Cracking Behavior
40%
Bond Coat
40%
Uncertainty Quantification
40%
Maximum Stress
37%
Oxide Thickness
35%
Parametric Study
30%
Computational Fluid Dynamics
30%
Compressor Rotor
28%
Compressor Performance
26%
Optimization Method
23%
Trailing Edge
20%
Electric Propulsion
20%
Axial Flow Fan
20%
Centrifugal Compressor
20%
Fe Analysis
20%
Ducted Propeller
20%
Air Mobility
20%
Propeller Design
20%
Winglets
20%
Aerodynamic Damping
20%
Axial Compressors
20%
Energy Management
20%
Backplate
20%
Temperature Fluctuation
20%
Steam Turbines
20%
Keyphrases
Fan Rotor
94%
Aerodynamic Performance
87%
Blade Curvature
61%
Multidisciplinary Design Optimization
61%
Robust Optimization
55%
Free-form Deformation
52%
Active Subspace
40%
Fan Stage
40%
Axial Fan
40%
Cracking Behavior
40%
Thermally Grown Oxide
40%
Interface Asperity
40%
Bond Coat
40%
Multi-objective Design Optimization
40%
Structural Constraints
40%
Transonic
40%
Total Pressure Ratio
38%
Freeform
35%
Sweeping
33%
Oxide Thickness
32%
Ducted Fan
30%
Turbofan
30%
Curvature Constraint
30%
Uncertainty Quantification
30%
Blade Twist
28%
Diffuser
27%
Compressor Performance
25%
Maximum Stress
25%
Aerodynamic Optimization
24%
Oxide Interfaces
24%
Flow Angle
24%
Chord Length
23%
Operating Conditions
23%
Trailing Edge
22%
Axial Compressor
20%
Turbocharger Compressor
20%
Clearance Effects
20%
Electric Aircraft Propulsion
20%
Forming Method
20%
Non-uniform Tip Clearance
20%
Hybrid-electric Aircraft
20%
Unsteady Shock Wave
20%
Static Stress
20%
Transonic Centrifugal Compressor
20%
Co-doped ZnO Thin Films
20%
Axial Flow Fan
20%
Highly Preferred Orientation
20%
FE Analysis
20%
Airfoil Aerodynamics
20%
Multi-fidelity Optimization
20%
