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西北工业大学 国内
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马 玉娥
Professor
航空学院
h-index
1096
引用
17
H-指数
根据储存在 Pure 的刊物以及来自 Scopus 的引用文献数量计算
2005
2025
每年的科研成果
综述
指纹
网络
科研成果
(111)
相似简介
(5)
指纹
深入其中 Yu'e Ma 为活跃的研究主题。这些主题标签来自此人的成果。它们共同形成唯一的指纹。
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Material Science
2024 Aluminium Alloy
29%
Aircraft
21%
Aluminum
44%
Aluminum Alloy
18%
Aluminum-Lithium Alloys
49%
Carbon Fiber
9%
Composite Laminate
9%
Composite Material
52%
Compression Load
9%
Compressive Strength
9%
Crack Arrest
10%
Crack Closure
12%
Crack Growth
64%
Crack Initiation
15%
Crack Propagation
24%
Creep
9%
Crystal Structure
19%
Damage Evolution
15%
Damage Tolerance
39%
Delamination
30%
Dynamic Fracture
9%
Fatigue Behavior
30%
Fatigue Crack
32%
Fatigue Crack Growth
76%
Fatigue of Materials
36%
Finite Element Method
32%
Finite Element Modeling
27%
Fracture Behavior
42%
Fracture Toughness
13%
Friction Stir Welding
20%
Glass Fiber
11%
Hyperelastic Material
9%
Large Deformation
14%
Laser Powder Bed Fusion
11%
Microhardness
10%
Phase Field Model
12%
Polymer Composite
9%
Reinforced Plastic
9%
Residual Stress
100%
Selective Laser Melting
12%
Stress Field
14%
Stress Intensity Factor
15%
Surface (Surface Science)
14%
Tensile Loads
13%
Tensile Property
14%
Three Dimensional Printing
14%
Ti-6Al-4V
14%
Titanium Alloy
16%
Ultimate Tensile Strength
8%
Welded Joint
26%
Engineering
Affected Zone
11%
Bridging
14%
Build Direction
14%
Crack Arrest
10%
Crack Growth
17%
Crack Growth Behavior
14%
Crack Growth Rate
44%
Crack Path
13%
Crack Propagation
11%
Damage Evolution
12%
Damage Tolerance
26%
Delamination Growth
10%
Dynamic Fracture
9%
Experimental Result
9%
Failure Mode
21%
Fatigue Behavior
33%
Fatigue Crack
13%
Fatigue Crack Growth
51%
Fatigue Crack Propagation
14%
Fatigue Life
18%
Fatigue Load
12%
Fatigue Performance
11%
Fatigue Property
16%
Fiber Metal Laminate
19%
Field Method
11%
Finite Element Analysis
28%
Finite Element Modeling
13%
Fracture Behavior
9%
Friction Stir Welding
10%
Joints (Structural Components)
44%
Laser Shock Peening
19%
Manufactured Ti6al4v
10%
Mixed Mode
9%
Peridynamics
12%
Phase Field
19%
Residual Stress
85%
Residual Stress Distribution
19%
Residual Stress Profile
11%
Retarders
14%
Selective Laser Melting
16%
Size Effect
14%
Spectral Decomposition
9%
Stiffened Panel
19%
Stress Field
12%
Stress-Intensity Factor
13%
T-Joints
9%
Tensile Property
11%
Tensiles
18%
Ti-6al-4v
19%
Weld
84%
