Keyphrases
Multidisciplinary Design Optimization
69%
Aerodynamic Performance
58%
Mistuning
55%
Low Speed Axial Compressor
55%
Museum Product
55%
Aeroelastic Characteristics
55%
Axial Compressor Rotor
55%
Measurement Dimension
55%
Curvature Constraint
55%
Aerodynamic Damping
55%
Souvenirs
55%
Historical museum
55%
Cultural Values
55%
Blade Curvature
55%
Creativity Assessment
55%
Product Creativity
55%
Interfacial Materials
55%
Electrical Contact Resistance
55%
Artificial Neural Network Modeling
55%
Numerical Methodology
55%
Thermoelectric Generator
55%
Fan Rotor
55%
Numerical Optimization
55%
Aerodynamics
55%
Design Optimization
55%
Thermal Contact Resistance
55%
Partially Connected
55%
Engine Order
55%
Exchange Strategy
55%
Spirometer
55%
Calibration-free
55%
High Precision Calibration
55%
Neural Network Optimization
55%
Multi-objective Grey Wolf Optimizer
55%
Axial Cooling Fan
55%
High Aspect Ratio Wing
55%
Variability Effects
55%
Geometric Variability
55%
Forced Response
41%
Blade Twist
41%
Amplitude Magnification
41%
Thermal Grease
37%
Heat Source Temperature
37%
Pressure Load
37%
Thermoelectric Generator System
37%
Heat Sink
37%
Artificial Neural Network Model
37%
Isentropic Efficiency
33%
Frequency Mistuning
27%
Forward Lean
27%
Von Mises Stress
27%
Total Pressure Ratio
27%
Maximum Stress
27%
Blade Tip Timing
27%
Aerodynamic Features
27%
Design Robustness
27%
Design Variability
27%
Multi-source Information
27%
Evaluation Costs
27%
Relative Evaluation
27%
Blade Performance
27%
Rotor
25%
Educational Level
18%
Cronbach
18%
Museum
18%
Structural Equation Analysis
18%
Creative Industries
18%
Selling
18%
Relevant Dimension
18%
Conceptual Model
18%
Moderating Effect
18%
Cultural Heritage Conservation
18%
Cultural Heritage Dissemination
18%
Cultural Novelty
18%
Scientific Rigor
18%
Instrument Validation
18%
Likert
18%
Exploratory Factor Analysis
18%
Systematization
18%
Overall Reliability
18%
Confirmatory Factor Analysis
18%
Cultural Industries
18%
Comprehensive Measure
18%
Generator Optimization
18%
Error Coefficient
18%
Measurement Model
18%
Low TCR
18%
China
18%
SmartPLS
18%
Online Survey
18%
Feedforward Neural Network
18%
Mean Square Error
18%
Thermal Conditions
18%
Mechanical Condition
18%
Thermoelectric Module
18%
Working Conditions
18%
Fully Connected
18%
Generator Design
18%
Correlation Coefficient
18%
Graphene Sheets
18%
Engineering
Aerodynamic Performance
100%
Pressure Ratio
83%
Compressor Rotor
77%
Rotors
69%
Isentropic Efficiency
66%
T Cell Receptor
55%
Aerodynamic Damping
55%
Axial Compressors
55%
Electrical Contact
55%
Maximum Stress
55%
Thermoelectrics
55%
Design Method
55%
Artificial Neural Network
55%
Gaseous Diffusion
55%
Effective Diffusivity
55%
Fiber Bragg Grating
55%
High Aspect Ratio
55%
Ducted Fan
55%
Fan Blade
55%
Unmanned Aerial Vehicle
55%
Computational Fluid Dynamics
48%
Force Response
41%
Interconnected Pore Space
37%
Optimization Method
33%
Multidisciplinary Design Optimization
33%
Finite Element Method
33%
Iteration Step
27%
Qubit
27%
Numerical Model
27%
Computational Load
27%
Optimization Strategy
27%
Design Process
27%
Aerodynamics
27%
Cost Evaluation
27%
Turbomachine Blades
27%
Uncertainty Quantification
27%
Information Source
27%
Freeform Deformation
25%
Heat Source
23%
Optimization Approach
23%
Streamwise
22%
Surrogate Model
22%
Design Space
20%
Baseline Blade
18%
Lift to Drag Ratio
18%
Winglets
18%
Grease
15%
Pressure Load
15%
Artificial Neural Network Model
15%
Aerodynamic Analysis
13%
Blade Tip
13%
Exit Flow
13%
Pressure Surface
13%
Backward Twist
13%
Twist Angle
13%
Rotor Blade
13%
Peak Efficiency
13%
Gaussians
13%
Prediction Error
13%
Service Life
13%
Structural Strength
11%
Strength Requirement
11%
Design Optimization
11%
Structural Performance
11%
Engineering
11%
Penalty Function
11%
Computational Cost
11%
Self-Organizing Map
11%
Performance Prediction
11%
Angle-of-Attack
9%
Time-of-Flight
9%
Research Work
9%
Flight Condition
9%
Propulsion System
9%
Power Engineering
9%
Battery Capacity
9%
Lift Coefficient
9%
Dominant Component
7%
Graphene Sheet
7%
Experimental Finding
7%
Feedforward
7%
Experimental Result
7%
Mean Square Error
7%
Design Generator
7%
Good Accuracy
7%
Equilibrium Moisture Content
6%
Testing Temperature
6%