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Gas Flow Development Through Tandem Heat Exchangers Inside Exhaust Nozzle by Using Porous Medium Model

Liu Xiyue Zhang Jingzhou Lou Decang Kang Yong

南京航空航天大学学报(英文版)2016,Vol.33Issue(2):147-154,8.
南京航空航天大学学报(英文版)2016,Vol.33Issue(2):147-154,8.

Gas Flow Development Through Tandem Heat Exchangers Inside Exhaust Nozzle by Using Porous Medium Model

Gas Flow Development Through Tandem Heat Exchangers Inside Exhaust Nozzle by Using Porous Medium Model

Liu Xiyue 1Zhang Jingzhou 1Lou Decang 2Kang Yong3

作者信息

  • 1. College of Energy and Power Engineering, Jiangsu Province Key Laboratory of Aerospace Power System,Nanjing University of Aeronautics and Astronautics, Nanjing 210016, P.R.China
  • 2. Collaborative Innovation Center of Advanced Aero-Engine, Beijing 100191, P.R.China
  • 3. China Gas Turbine Establishment, Chengdu 610500, P.R.China
  • 折叠

摘要

关键词

compact heat exchanger/exhaust nozzle/porous medium/pressure loss/numerical simulation

Key words

compact heat exchanger/exhaust nozzle/porous medium/pressure loss/numerical simulation

分类

航空航天

引用本文复制引用

Liu Xiyue,Zhang Jingzhou,Lou Decang,Kang Yong..Gas Flow Development Through Tandem Heat Exchangers Inside Exhaust Nozzle by Using Porous Medium Model[J].南京航空航天大学学报(英文版),2016,33(2):147-154,8.

南京航空航天大学学报(英文版)

OACSCDCSTPCD

1005-1120

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