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西北工业大学 国内
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科研成果
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屈 峰
Professor
航空学院
h-index
887
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
2014
2025
每年的科研成果
综述
指纹
网络
科研成果
(87)
相似简介
(4)
指纹
深入其中 Feng Qu 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。
分类
加权
按字母排序
Engineering
Airfoil
100%
Two Dimensional
93%
Vortex
77%
Numerical Experiment
71%
Computational Fluid Dynamics
69%
Aerodynamics
68%
High Resolution
57%
One Dimensional
55%
Thermal Load
52%
Design Optimization
52%
Euler Equation
49%
Turbulent Flow
46%
Boundary Layer
43%
Numerical Study
43%
Mass Transport
41%
Aerodynamic Shape Optimization
41%
Oscillatory
36%
Streamwise
35%
Separation Bubble
35%
Mach Number
33%
Flow Separation
33%
Design Condition
32%
Space Vehicle
30%
Elliptical Shape
30%
Hypersonic Flows
29%
Spherical Coordinate
28%
Isotropic Turbulence
28%
Aspect Ratio
28%
Layer Interaction
27%
Flow Distribution
26%
Shear Layer
24%
Compressible Flow
24%
Shear Wave
24%
Section Reduction
24%
Radar Cross Section
24%
Deep Learning Method
24%
Performance Analysis
24%
Limiters
24%
Simulation Method
24%
Aerodynamic Performance
23%
Design Method
23%
Optimization Method
22%
Reynolds-Averaged Navier-Stokes
22%
Inviscid Flow
22%
Viscous Flow
21%
Thermal Protection
20%
System Protection
20%
Flow Structure
20%
Drag Divergence
20%
Aerodynamic Design
20%
Physics
Hypersonics
85%
Spherical Coordinate
43%
Airfoil
40%
High Resolution
34%
Turbulent Flow
30%
Space Vehicle
24%
S Wave
24%
Computational Fluid Dynamics
19%
Conservation Law
18%
Supersonics
18%
Hypersonic Flow
18%
Flat Plate
16%
Laminar Boundary Layer
16%
Shear Layer
16%
Shock Tubes
14%
Elastic Wave
13%
Flow Control
12%
Boundary Layer Transition
12%
Supersonic Boundary Layer
12%
Astronautics
12%
Compressible Flow
12%
Inviscid Flow
12%
Finite Difference Method
12%
Shock Wave Interaction
12%
Aerodynamic Heating
12%
Reentry Vehicle
12%
Base Flow
12%
Blast Wave
12%
Boundary Layer
10%
Viscous Flow
10%
Reynolds Number
9%
Mach Reflection
7%
Shock Wave
7%
Wall Jet
6%
Transport Theory
6%
Spatial Distribution
6%
Vorticity
6%
Instability Phenomenon
6%
Traveling Wave
6%
Compressibility
6%
