• 其他栏目

    王成鹏

    • 教授 博士生导师
    • 招生学科专业:
      力学 -- 【招收博士、硕士研究生】 -- 航空学院
      航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 航空学院
      航空宇航科学与技术 -- 【招收硕士研究生】 -- 航空学院
      机械 -- 【招收博士、硕士研究生】 -- 航空学院
    • 性别:男
    • 所在单位:航空学院
    • 办公地点:明故宫校区流体楼C12-409
    • 联系方式:wangcp@nuaa.edu.cn 025-84896323
    • 电子邮箱:

    访问量:

    开通时间:..

    最后更新时间:..

    A study on the RR-to-MR transition of shock wave reflections near the leading edge in hypersonic flows

    点击次数:

    所属单位:航空学院

    教研室:高速风洞实验室

    发表刊物:J. Fluid Mech.

    刊物所在地:Cambridge University Press

    项目来源:国家自然科学基金

    关键字:flow–structure interactions, high-speed flow, boundary-layer separation

    摘要:In this paper, the incident shock–separation shock interactions on a surface plate near the leading edge are studied theoretically and experimentally, and the transition from regular reflection (RR) to Mach reflection (MR) is the main focus. The theoretical method employs free interaction theory (FIT) and the minimum entropy production (MEP) principle to analyse the separation shock strength of flow separated from the boundary layer and separated from the leading edge, respectively, the criterion based on the MEP principle is employed to predict the RR-to-MR transition near the leading edge. The experiments were performed on a rotatable wedge situated over a sharp leading-edge plate such that the wedge could continuously change the flow deflection angle from 0◦ to 40◦ by means of a high-precision control device. Fast-response transducers and a high-speed camera were used to measure dynamic pressures and to take schlieren images, respectively. The influences of wedge positions, Reynolds

    论文类型:期刊论文

    论文编号:doi:10.1017/jfm.2021.421

    学科门类:工学

    一级学科:力学

    卷号:919

    期号:A40

    页面范围:A40 1-21

    ISSN号:0022-1120

    是否译文:

    发表时间:2021-06-01