Keyphrases
ARX Model
50%
Bi-modulus Material
50%
Bimodulus
50%
Cantilever Beam
100%
Car Engine
50%
Cement Industry
50%
Commercial Vehicle
50%
Consumption Emissions
50%
Durability Test
50%
Elastic Cantilever
50%
End Moments
50%
Finite Element Analysis
50%
Fixed-wing Unmanned Aerial Vehicles
100%
Fuel Consumption
58%
Fuel NO
50%
Functionally Graded
100%
Functionally Graded Materials
83%
Gear Materials
50%
Gearbox
50%
Hollow
50%
Horizontal Deflection
50%
Hydraulic Valve
50%
Large Deflection
100%
Medium-duty Truck
50%
Mixing Process
50%
Model Predictive Controller
83%
NO Emission
50%
Nonlinear Elasticity
50%
Numerical Results
65%
Operating Condition Effects
50%
Orthotropic
75%
Plastic Anisotropy
66%
Processor-in-the-loop Test
50%
Railway Axle
50%
Rotating Bending
50%
Shrink Fit
50%
Solid Disk
50%
Spark Ignition Engine
50%
Spot Welding
50%
Stress Concentration
50%
Stress Intensity Factor Solution
50%
Time Series Methods
50%
Transverse Magnetic Field
50%
Truck Diesel Engine
50%
Valve Lifter
50%
Variable Thickness
50%
Vertical Deflection
50%
Viscoelastic Wave
50%
Wave Characteristics
50%
Windy Condition
50%
Engineering
Accelerated Fatigue Test
33%
Anisotropic
50%
Approximate Solution
50%
Biaxial Tension
50%
Cantilever Beam
100%
Circular Hole
50%
Commercial Vehicle
50%
Cost Reduction
50%
Crack Shape
33%
Diesel Engine
50%
Dynamometer
33%
End Moment
50%
Fatigue Life
50%
Feed Rate
50%
Finite Element Method
73%
Fixed Wings
100%
Flow Rule
50%
Flying Quality
37%
Functionally Graded Material
100%
Gap Value
50%
Gearbox
50%
Hardenability
33%
Hydraulics
50%
Hypoid Gear
50%
Internal Combustion Engine
87%
Load Condition
40%
Magnetic Field
50%
Material Behavior
50%
Material Component
50%
Material Optimisation
50%
Moving Average
50%
Multi-Input Multi-Output
37%
Multiple-Input Multiple-Output
50%
Natural Frequency
50%
Part Load
50%
Pinion
50%
Plastic Flow
50%
Process Control
50%
Radial Stress
50%
Railway
50%
Road
33%
Root Mean Square Error
37%
Shrink Fit
50%
Solution Technique
50%
Steady Heading
37%
Stress Concentration
50%
Stress Concentration Factor
50%
Stress-Intensity Factor
50%
Test Rig
33%
Unmanned Aerial Vehicle
100%
