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Component Matching Based on Low Bypass Ratio Mixed Exhaust Turbofan Engine

Zheng Xilong Wu Tieying Ji Honghu

南京航空航天大学学报（英文版）2018，Vol.35Issue(5)：9-15,7.
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南京航空航天大学学报（英文版）2018，Vol.35Issue(5)：9-15,7.

Component Matching Based on Low Bypass Ratio Mixed Exhaust Turbofan Engine

Component Matching Based on Low Bypass Ratio Mixed Exhaust Turbofan Engine

Zheng Xilong 1Wu Tieying 1Ji Honghu1

作者信息

  • 1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China
  • 折叠

摘要

关键词

turbofan engine/low bypass ratio/off-design/component matching/OOP/performance analysis

Key words

turbofan engine/low bypass ratio/off-design/component matching/OOP/performance analysis

分类

航空航天

引用本文复制引用

Zheng Xilong,Wu Tieying,Ji Honghu..Component Matching Based on Low Bypass Ratio Mixed Exhaust Turbofan Engine[J].南京航空航天大学学报（英文版）,2018,35(5):9-15,7.

基金项目

This work was supported in part by the Fundamental Research Funds for the Central Universities (No.NZ2016103). （No.NZ2016103）

南京航空航天大学学报（英文版）

OACSCDCSTPCD

1005-1120

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