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西北工业大学 国内
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Effect of serpentine nozzle on bypass ratio of turbofan engine exhaust
Peng Sun,
Li Zhou
,
Zhan Xue Wang
, Xiao Lin Sun
动力与能源学院
Northwestern Polytechnical University Xian
科研成果
:
书/报告/会议事项章节
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会议稿件
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同行评审
4
引用 (Scopus)
综述
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探究 'Effect of serpentine nozzle on bypass ratio of turbofan engine exhaust' 的科研主题。它们共同构成独一无二的指纹。
分类
加权
按字母排序
Engineering
Convergent
100%
Turbofan Engine
100%
Bypass Ratio
100%
Exhaust Systems (Engine)
100%
Axisymmetric
90%
Mixers (Machinery)
30%
Duct
20%
Core Flow
20%
Turbine
10%
Pressure Gradient
10%
Boundary Condition
10%
Flow Characteristic
10%
Streamlines
10%
Mass Transport
10%
Infrared Radiation
10%
Survivability
10%
Inlet Nozzle
10%
Earth and Planetary Sciences
Turbofan Engine
100%
Convergent Nozzle
100%
Core Flow
22%
Flow Characteristic
11%
Pressure Gradient
11%
Mass Transport
11%
Boundary Condition
11%
Turbine Engine
11%
Infrared Radiation
11%