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Characteristics and mechanisms of turboshaft engine axial compressor casing containment

机译:涡轮轴发动机轴流式压缩机套管壳体的特性和机制

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  • 来源
    《中国航空学报(英文版)》 |2021年第1期|171-180|共10页
  • 作者单位

    College of Energy Engineering Zhejiang University Hangzhou 310027 China;

    Collaborative Innovation Center for Advanced Aero-engine Beijing 100083 China;

    AECC Hunan Aviation Powerplant Research Institute Zhuzhou 410002 China;

    College of Energy Engineering Zhejiang University Hangzhou 310027 China;

    Collaborative Innovation Center for Advanced Aero-engine Beijing 100083 China;

    AECC Hunan Aviation Powerplant Research Institute Zhuzhou 410002 China;

    College of Energy Engineering Zhejiang University Hangzhou 310027 China;

    Collaborative Innovation Center for Advanced Aero-engine Beijing 100083 China;

    College of Energy Engineering Zhejiang University Hangzhou 310027 China;

    Collaborative Innovation Center for Advanced Aero-engine Beijing 100083 China;

    College of Energy Engineering Zhejiang University Hangzhou 310027 China;

    Collaborative Innovation Center for Advanced Aero-engine Beijing 100083 China;

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  • 正文语种 eng
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