Keyphrases
Aerodynamic Analysis
17%
Aerodynamic Characteristics
17%
Aerodynamic Damping
71%
Aerodynamic Performance
75%
Aerodynamics
71%
Aeroelastic Analysis
17%
Aeroelastic Characteristics
71%
Aeroelastic Performance
17%
Amplitude Magnification
53%
Artificial Neural Network Model
47%
Artificial Neural Network Modeling
71%
Axial Compressor Rotor
71%
Blade Aerodynamics
17%
Blade Curvature
71%
Blade Tip
17%
Blade Twist
53%
China
23%
Comprehensive Measure
23%
Conceptual Model
23%
Confirmatory Factor Analysis
23%
Correlation Coefficient
23%
Creative Industries
23%
Creativity Assessment
71%
Cronbach
23%
Cultural Heritage Conservation
23%
Cultural Heritage Dissemination
23%
Cultural Industries
23%
Cultural Novelty
23%
Cultural Values
71%
Curvature Constraint
71%
Deformation Process
17%
Design Optimization
71%
Educational Level
23%
Electrical Contact Resistance
71%
Error Coefficient
23%
Exit Routes
17%
Exploratory Factor Analysis
23%
Fan Rotor
71%
Feedforward Neural Network
23%
Finite Element Method
21%
Flow Angle
17%
Flutter
17%
Forced Response
53%
Forward Lean
35%
Frequency Mistuning
35%
Fully Connected
23%
Gaussian Process
17%
Generator Design
23%
Generator Optimization
23%
Good Accuracy
23%
Graphene Sheets
23%
Heat Sink
47%
Heat Source Temperature
47%
High Temperature
23%
Historical museum
71%
In-house Code
17%
Instrument Validation
23%
Interfacial Materials
71%
Isentropic Efficiency
42%
Kriging
17%
Likert
23%
Low Speed Axial Compressor
71%
Low TCR
23%
Maximum Stress
35%
Mean Square Error
23%
Measurement Dimension
71%
Measurement Model
23%
Mechanical Condition
23%
Mistuning
71%
Moderating Effect
23%
Multidisciplinary Design Optimization
89%
Museum
23%
Museum Product
71%
Numerical Methodology
71%
Numerical Optimization
71%
Online Survey
23%
Optimization Approach
17%
Overall Reliability
23%
Pressure Load
47%
Pressure Surface
17%
Product Creativity
71%
Relevant Dimension
23%
Response Mean
17%
Rotor
32%
Rotor Blade
17%
Scientific Rigor
23%
Selling
23%
SmartPLS
23%
Souvenirs
71%
Structural Equation Analysis
23%
Systematization
23%
Thermal Conditions
23%
Thermal Contact Resistance
71%
Thermal Grease
47%
Thermoelectric Generator
71%
Thermoelectric Generator System
47%
Thermoelectric Module
23%
Total Pressure Ratio
35%
Von Mises Stress
35%
Working Conditions
23%
Engineering
Aerodynamic Analysis
17%
Aerodynamic Damping
71%
Aerodynamic Performance
92%
Artificial Neural Network
71%
Artificial Neural Network Model
20%
Axial Compressors
71%
Backward Twist
17%
Blade Tip
17%
Compressor Rotor
100%
Computational Cost
14%
Computational Fluid Dynamics
14%
Design Generator
10%
Design Method
71%
Design Optimization
14%
Design Space
14%
Dominant Component
10%
Electrical Contact
71%
Engineering
14%
Equilibrium Moisture Content
7%
Exit Flow
17%
Experimental Finding
10%
Experimental Result
10%
Feedforward
10%
Finite Element Method
42%
Force Response
53%
Freeform Deformation
32%
Gaussians
17%
Good Accuracy
10%
Graphene Sheet
10%
Grease
20%
Heat Source
30%
Isentropic Efficiency
50%
Maximum Stress
71%
Mean Square Error
10%
Multidisciplinary Design Optimization
42%
Optimization Approach
17%
Optimization Method
42%
Peak Efficiency
17%
Penalty Function
14%
Performance Prediction
14%
Pressure Load
20%
Pressure Ratio
35%
Pressure Surface
17%
Rotor Blade
17%
Rotors
89%
Self-Organizing Map
14%
Streamwise
28%
Strength Requirement
14%
Structural Performance
14%
Structural Strength
14%
Surrogate Model
28%
T Cell Receptor
71%
Testing Temperature
7%
Thermoelectrics
71%
Twist Angle
17%