Engineering
Aerodynamic Performance
100%
Rotors
94%
Pressure Ratio
86%
Ducted Fan
56%
Design Optimization
54%
Turbomachine Blades
50%
Freeform Deformation
47%
Optimization Strategy
45%
Surrogate Model
45%
Chord Length
45%
Multidisciplinary Design Optimization
44%
Uncertainty Quantification
41%
Optimization Approach
40%
Compressor Rotor
40%
Multiobjective Optimization
39%
Optimum Design
38%
Leakage Flow
38%
Exit Flow
38%
Multiobjective Genetic Algorithm
38%
Aerodynamics
36%
Computational Fluid Dynamics
36%
Finite Element Method
35%
Pressure Loss Coefficient
33%
Shock Strength
33%
Structural Constraint
33%
Diffusers
33%
Covariance Matrix
33%
Singular Value Decomposition
33%
Design Stage
33%
Cracking Behavior
33%
Bond Coat
33%
Axial Compressors
33%
Maximum Stress
31%
Oxide Thickness
29%
Force Response
29%
Fan Blade
28%
Parametric Study
25%
Winglets
22%
Compressor Performance
21%
Isentropic Efficiency
20%
Optimization Method
19%
Unmanned Aerial Vehicle
19%
Trailing Edge
17%
Electric Propulsion
16%
Axial Flow Fan
16%
Centrifugal Compressor
16%
Fe Analysis
16%
Air Mobility
16%
Propeller Design
16%
Aerodynamic Damping
16%
Keyphrases
Aerodynamic Performance
81%
Fan Rotor
79%
Multidisciplinary Design Optimization
55%
Blade Curvature
50%
Robust Optimization
46%
Free-form Deformation
43%
Total Pressure Ratio
40%
Active Subspace
33%
Fan Stage
33%
Axial Fan
33%
Cracking Behavior
33%
Thermally Grown Oxide
33%
Interface Asperity
33%
Bond Coat
33%
Multi-objective Design Optimization
33%
Structural Constraints
33%
Transonic
33%
Mistuning
33%
Axial Compressor Rotor
33%
Engine Order
33%
Freeform
29%
Forced Response
29%
Sweeping
28%
Oxide Thickness
27%
Ducted Fan
25%
Turbofan
25%
Curvature Constraint
25%
Uncertainty Quantification
25%
Amplitude Magnification
25%
Blade Twist
24%
Operating Conditions
24%
Diffuser
22%
Compressor Performance
21%
Maximum Stress
21%
Design Optimization
21%
Aerodynamic Optimization
20%
Oxide Interfaces
20%
Flow Angle
20%
Chord Length
19%
Trailing Edge
18%
Coupling Effect
18%
Axial Compressor
16%
Turbocharger Compressor
16%
Clearance Effects
16%
Electric Aircraft Propulsion
16%
Forming Method
16%
Non-uniform Tip Clearance
16%
Hybrid-electric Aircraft
16%
Unsteady Shock Wave
16%
Static Stress
16%
