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西北工业大学 国内
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动力与能源学院
西北工业大学
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指纹
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简介
(19)
科研成果
(2598)
指纹
深入其中 动力与能源学院 为活跃的研究主题。这些主题标签来自该组织中成员的成果。它们共同形成唯一的指纹。
分类
加权
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Engineering
Rotors
100%
Flow Distribution
84%
Turbine
78%
Experimental Investigation
71%
Vortex
64%
Aero-Engines
53%
Axial-Flow Compressors
53%
Casing Treatment
53%
Leading Edge
52%
Axial Compressors
51%
Pulse Detonation Engine
43%
Heat Transfer Coefficient
41%
Aerodynamic Performance
38%
Pressure Ratio
38%
Cooling Performance
37%
Leakage Flow
37%
Reynolds' Number
35%
Blade Tip
34%
Combustor
33%
Transients
33%
Suction Surface
32%
Blade Turbine
31%
Compressor Rotor
30%
Numerical Study
29%
Aeroengine
29%
Flow Characteristic
29%
Secondary Flow
27%
Rocket Engine
26%
Aerodynamics
26%
Experimental Result
25%
Detonation Wave
25%
Circumferential
23%
Turbofan Engine
20%
Trailing Edge
20%
Simulation Result
19%
Compressor Performance
19%
Design Optimization
19%
Flow Velocity
19%
Ignition
19%
Guide Vane
19%
Unsteady Flow
18%
Cooling Hole
18%
Engine Performance
18%
Discharge Coefficient
17%
Flow Mechanism
17%
Axisymmetric
17%
Boundary Layer Suction
17%
Boundary Layer
17%
Flow Rate
17%
Deflagration
17%
Pressure Loss
17%
Control System
17%
Flow Separation
16%
Computational Fluid Dynamics
16%
Rotor System
16%
Design Method
16%
Engine Cycle
16%
Flow Structure
15%
Suction Side
15%
Liquid Crystal
15%
Failure Probability
14%
Pressure Sensitive Paint
14%
Mass Flowrate
14%
Pressure Side
14%
Pressure Surface
14%
Mach Number
14%
Oxidizer
13%
Transition to Detonation
13%
Turbulence Intensity
13%
Fault Diagnosis
13%
Compressor Blade
13%
Convergent
13%
Design Point
13%
Impeller
13%
Tunnel
13%
Incidence Angle
12%
Temperature Distribution
12%
Numerical Method
12%
Rotor Blade
12%
Blade Surface
12%
Pressure Distribution
11%
Duct
11%
Reliability Analysis
11%
Diffusers
11%
Main Flow
11%
Air Flow
11%
Centrifugal Pump
11%
Simulation Method
11%
Flow Loss
11%
Static Pressure
10%
Rotating Speed
10%
Peak Efficiency
10%
Nusselt Number
10%
Optimization Method
10%
Airfoil
10%
Two Dimensional
9%
Breathing
9%
Equivalence Ratio
9%
Operating Frequency
9%
Centrifugal Compressor
9%