Engineering
Aerodynamic Damping
17%
Aerodynamic Performance
96%
Aerodynamics
29%
Air Mobility
17%
Axial Compressors
35%
Axial Flow Fan
17%
Backplate
17%
Bond Coat
35%
Centrifugal Compressor
17%
Chord Length
47%
Compressor Performance
23%
Compressor Rotor
42%
Computational Fluid Dynamics
26%
Covariance Matrix
35%
Cracking Behavior
35%
Design Optimization
57%
Design Stage
35%
Diffusers
35%
Ducted Fan
41%
Electric Propulsion
17%
Energy Management
17%
Exit Flow
40%
Fe Analysis
17%
Finite Element Method
37%
Force Response
31%
Freeform Deformation
49%
Leakage Flow
40%
Maximum Stress
33%
Multidisciplinary Design Optimization
46%
Multiobjective Genetic Algorithm
40%
Multiobjective Optimization
41%
Optimization Approach
40%
Optimization Method
20%
Optimization Strategy
39%
Optimum Design
40%
Oxide Thickness
31%
Parametric Study
26%
Pressure Loss Coefficient
35%
Pressure Ratio
73%
Propeller Design
17%
Rotors
100%
Shock Strength
35%
Singular Value Decomposition
35%
Structural Constraint
35%
Surrogate Model
48%
Temperature Fluctuation
17%
Trailing Edge
18%
Turbomachine Blades
44%
Uncertainty Quantification
35%
Winglets
17%
Keyphrases
Active Subspace
35%
Aerodynamic Optimization
21%
Aerodynamic Performance
85%
Amplitude Magnification
26%
Axial Compressor
17%
Axial Compressor Rotor
35%
Axial Fan
35%
Blade Curvature
53%
Blade Twist
25%
Bond Coat
35%
Chord Length
20%
Clearance Effects
17%
Compressor Performance
22%
Coupling Effect
19%
Cracking Behavior
35%
Curvature Constraint
26%
Design Optimization
22%
Diffuser
23%
Ducted Fan
26%
Electric Aircraft Propulsion
17%
Engine Order
35%
Fan Rotor
83%
Fan Stage
35%
Flow Angle
21%
Forced Response
31%
Forming Method
17%
Free-form Deformation
46%
Freeform
31%
Hybrid-electric Aircraft
17%
Interface Asperity
35%
Maximum Stress
22%
Mistuning
35%
Multi-objective Design Optimization
35%
Multidisciplinary Design Optimization
58%
Non-uniform Tip Clearance
17%
Operating Conditions
25%
Oxide Interfaces
21%
Oxide Thickness
28%
Robust Optimization
49%
Static Stress
17%
Structural Constraints
35%
Sweeping
29%
Thermally Grown Oxide
35%
Total Pressure Ratio
43%
Trailing Edge
19%
Transonic
35%
Turbocharger Compressor
17%
Turbofan
26%
Uncertainty Quantification
26%
Unsteady Shock Wave
17%