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    黄向华

    • 教授 博士生导师
    • 招生学科专业:
      动力工程及工程热物理 -- 【招收博士、硕士研究生】 -- 能源与动力学院
      航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 能源与动力学院
      能源动力 -- 【招收博士、硕士研究生】 -- 能源与动力学院
    • 毕业院校:南京航空航天大学
    • 学历:南京航空航天大学
    • 学位:工学博士学位
    • 所在单位:能源与动力学院
    • 联系方式:xhhuang@nuaa.edu.cn
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    Modeling and Assessment of a Contra-Rotating Puller Propfan Engine

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    所属单位:能源与动力学院

    发表刊物:Tuijin Jishu

    摘要:In order to analyze the performance of propfan engines to provide methods for beforehand research, a simulation model of three-shaft contra-rotating puller propfan was proposed. Propfan engine was considered as a match with propfan and turboshaft. Propfan model, based on the similitude principle, starts with the aerodynamic performance for a single rotating propfan. The influence of hub, the interaction of contra-rotating propfans and the contraction of stream are all considered. Error of the model and the experimental results is no more than 2%. The core engine model is a component-level model of a three-shaft turboshaft. Assessments are conducted based on the model. The propfan-inlet interaction has a little influence on performance and could be ignored. The wheelbase of contra-rotating to radius ratio may have an impact on performance and could be set up from 0.4 to 0.6. When the pitch angles are both 56°, the thrust would decrease and sfc would increase if the height grows up. If the Mach number grows up, sfc would increase first and then decrease, and the thrust would decrease first and then increase. The pitch angles of propfan are important regulative parameters for engine performance. When the variations of pitch angles are 4°, the thrust will change 64%. © 2018, Editorial Department of Journal of Propulsion Technology. All right reserved.

    ISSN号:1001-4055

    是否译文:

    发表时间:2018-02-01

    合写作者:Wang, Yi-Wei

    通讯作者:黄向华