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