Material Science
Aircraft
8%
Aluminum Alloys
17%
Bimetal
8%
Carbide
16%
Carbon Fiber
8%
Cast Aluminum Alloy
30%
Cast Iron
17%
Coarsening
53%
Constitutive Modeling
8%
Corrosion
8%
Crack Growth
21%
Crack Initiation
18%
Crack Propagation
25%
Damage Evolution
23%
Elastic Constant
8%
Fatigue Behavior
23%
Fatigue Crack
24%
Fatigue of Materials
73%
Finite Element Method
19%
Fracture Mechanics
12%
Grain Boundary
14%
Grain Size
13%
Heat Treatment
8%
High Strength Steels
8%
High-Cycle Fatigue
20%
High-Temperature Fatigue
8%
Low-Cycle Fatigue
21%
Materials Property
10%
Mechanical Degradation
8%
Mechanical Property
13%
Mechanical Strength
11%
Micromechanics
8%
Nickel-Based Superalloys
100%
Nucleation
16%
Powder Metallurgy
17%
Sand Casting
8%
Scanning Electron Microscopy
11%
Short Crack
14%
Silicon Alloys
34%
Single Crystal
21%
Small Crack
24%
Stress Concentration
8%
Stress-Strain Relations
8%
Superalloys
85%
Tensile Property
19%
Thermal Barrier Coatings
8%
Two Phase Flow
8%
Ultimate Tensile Strength
12%
Vickers Hardness
18%
Yield Stress
13%
Engineering
Aero-Engines
11%
Aircraft Engine
8%
Aluminum Castings
8%
Applied Stress
8%
Arm Spacing
19%
Barrier Coating
8%
Blade Turbine
56%
Carbon Fibre Composite
8%
Cast Iron
8%
Coating System
8%
Constitutive Model
17%
Constitutive Modeling
17%
Corrosion Fatigue
8%
Corrosion Mechanism
8%
Crack Growth
8%
Cylinder Heads
53%
Damage Analysis
8%
Damage Evolution
11%
Damage Variable
8%
Defects
13%
Design Requirement
8%
Diesel Engine
17%
Elastic Constant
8%
Elevated Temperature
18%
Engine Cylinders
26%
Exhaust Manifolds
8%
Exhaust Systems (Engine)
8%
Experimental Investigation
8%
Failure Analysis
17%
Fatigue Crack Propagation
8%
Fatigue Life
34%
Fatigue Modeling
8%
Fatigue Property
12%
Finite Element Method
9%
High Cycle Fatigue
20%
High Strength Steel
8%
High Temperature Effect
8%
Laser Shock Peening
8%
Microstructure
71%
Nickel Powder Metallurgy
8%
Phase Field
8%
Porosity
15%
Property Degradation
9%
Quantile Regression Neural Network
8%
Service Process
9%
Strengthening Mechanism
10%
Tensile Property
17%
Tensiles
11%
Thermal Barrier
8%
Thermal Exposure
8%
