学者信息

施崇广

航空航天学院

合作者

已发表成果:

WOK 论文 11 篇;中文核心 6 篇;其它论文 5 篇;

  • A unified transition mechanism from shock to detonation waves

    arXiv,,2024-08-06.
    Yan, Hao (1); Xiong, Haochen (1); Han, Xin (1); Shi, Chongguang (1); You, Yancheng (1)
    EI:20240345247   10.48550/arXiv.2408.03042
    收录情况:EI
  • Fully appreciating the impossibility of shock wave regular reflection from the axis of symmetry in axisymmetric internal flows

    Physics of Fluids,1070-6631,2024-07-01.
    Zhang, Tao (1); Hu, Waner (1); Da, Xingya (2); Shi, Chongguang (1); Zhu, Chengxiang (1); You, Yanch...
    EI:20242916718760   10.1063/5.0220314
    收录情况:EI
  • A theoretical method for oblique and curved detonation waves

    PHYSICS OF FLUIDS,1070-6631,2024-06.
    Yan, Hao; Xiong, Haochen; Han, Xin; Shi, Chongguang; You, Yancheng
    WOS:001239606400013   EI:20242416258149   10.1063/5.0210780
    收录情况:SCIE、EI
  • Curved detonation and its reflections

    JOURNAL OF FLUID MECHANICS,0022-1120,2024-04-01.
    Yan, Hao; Han, Xin; Xiong, Haochen; Shi, Chongguang; You, Yancheng
    WOS:001194219300001   EI:20241515882213   10.1017/jfm.2024.142
    收录情况:SCIE、EI
  • Analytical reconstruction of axisymmetric curved shock wave/boundary layer interactions

    Physics of Fluids,1070-6631,2024-04-01.
    Cheng, Jianrui; Zhang, Tao; Shi, Chongguang; Da, Xingya; Zhu, Chengxiang; You, Yancheng
    WOS:001209401100014   EI:20241916033334   10.1063/5.0199292
    收录情况:SCIE、EI
  • 真实气体效应下前体/进气道一体化模型气动特性研究

    推进技术,1001-4055,2024-12-17.
    粟荣广;韩信;胡占仓;施崇广;尤延铖
    CSCD核心库
  • 考虑巡航攻角的三维内转进气道设计与分析

    航空学报,1000-6893,2024-12-02.
    郑晓刚;胡占仓;蔡泽君;施崇广;朱呈祥;尤延铖
    CSCD核心库
  • 高超声速三维内转进气道研究进展综述

    航空学报,1000-6893,2024-12-02.
    郑晓刚;施崇广;张加乐;张咪;朱文磊;朱呈祥;尤延铖
    CSCD核心库
  • 侧滑角对V型钝化唇口激波干扰结构影响研究

    航空学报,1000-6893,2024-06-30.
    饶洛瑜;张涛;施崇广;朱呈祥;尤延铖
    CSCD核心库
  • 三维弯曲流面法及其在外流乘波体中的应用

    航空学报,1000-6893,2024-06-19.
    杨凯;张勐飞;施崇广;余耀堃;郑晓刚;朱呈祥;尤延铖
    CSCD核心库