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Numerical study on aerodynamic performance of multi-stage lobed mixer-ejector
更新时间:2026-07-07
    • Numerical study on aerodynamic performance of multi-stage lobed mixer-ejector

    • Vol. 31, Issue 3, Pages: 631-638(2016)
    • DOI:10.13224/j.cnki.jasp.2016.03.014    

      CLC:
    • Published:2016

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  • doi: 10.13224/j.cnki.jasp.2016.03.014 DOI:

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Related Author

LIU You-hong
XIE Yi
GUO Nan
HUANG Shuai
XU Jinglei
WANG Yangsheng
XIE Jian-guang
HUANG Yi-yong

Related Institution

School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
China Gas Turbine Establishment, Aviation Industry Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Power and Energy Engineering, Beijing University of Aeronautics and Astronautics
Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
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