Numerical study of pressurization and flow characteristics of rotating detonation combustor by channel configuration and outlet contraction ratio

被引:0
|
作者
Chen, Zhanming [1 ]
Huang, Lvmeng [1 ]
Xu, Jinxuan [1 ]
Yang, Zhao [2 ]
机构
[1] Shaanxi Key Laboratory of New Transportation Energy and Automotive Energy Saving, Chang'an University, Xi'an,710064, China
[2] National Key Laboratory of Aeronautical Power System and Plasma Technology, Air Force Engineering University, Shaanxi, Xi ’an,710051, China
关键词
D O I
10.1016/j.ijheatfluidflow.2025.109764
中图分类号
学科分类号
摘要
Detonation
引用
收藏
相关论文
共 50 条
  • [1] Thermodynamic Analysis on Pressurization Characteristics of Continuously Rotating Detonation Combustor
    Zheng, Hong-Tao
    Qi, Lei
    Zhao, Ning-Bo
    Liu, Shi-Zheng
    [J]. Tuijin Jishu/Journal of Propulsion Technology, 2018, 39 (05): : 1057 - 1066
  • [2] Influence of equivalence ratio on characteristics of continuously rotating detonation combustor
    当量比对连续旋转爆轰燃烧室特性的影响
    [J]. Zhao, Ningbo (zhaoningboheu@126.com), 2018, Beijing University of Aeronautics and Astronautics (BUAA) (33):
  • [3] Numerical investigation on flow and film cooling characteristics of coolant injection in rotating detonation combustor
    Tian, Jia
    Wang, Yuan-shuai
    Zhang, Jing-zhou
    Tan, Xiao-ming
    [J]. EUROPEAN POLYMER JOURNAL, 2023, 189
  • [4] Numerical investigation on flow and film cooling characteristics of coolant injection in rotating detonation combustor
    Tian, Jia
    Wang, Yuan-shuai
    Zhang, Jing-zhou
    Tan, Xiao-ming
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 122
  • [5] Numerical investigation on flow and film cooling characteristics of coolant injection in rotating detonation combustor
    Tian, Jia
    Wang, Yuan-shuai
    Zhang, Jing-zhou
    Tan, Xiao-ming
    [J]. Aerospace Science and Technology, 2022, 122
  • [6] Pressurization Characteristics and Flow Field Analysis of Methane/Oxygen Rotating Detonation Combustor at High Temperature and High Pressure Inlets
    Sun, Zhi-Peng
    Huang, Yue
    Luan, Zhen-Ye
    Gao, Si-Jia
    You, Yan-Cheng
    [J]. Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (11):
  • [7] Numerical Investigation on Heat Transfer Characteristics of a Rotating Detonation Combustor Wall
    Qiu, Yan-Ming
    Wu, Yu-Wen
    Kang, Chao-Hui
    Lei, Te
    Li, Qun
    Xu, Gao
    Weng, Chun-Sheng
    [J]. Tuijin Jishu/Journal of Propulsion Technology, 2023, 44 (10):
  • [8] Numerical Study on Aerodynamic Performance of Turbine for Rotating Detonation Combustor
    Meng, Bo-Wei
    Yang, Bo
    Zhang, Cui-Zhen
    Wang, Feng-Ming
    Ma, Hu
    Xia, Zhen-Juan
    Zhou, Chang-Sheng
    [J]. Tuijin Jishu/Journal of Propulsion Technology, 2023, 44 (09):
  • [9] Three-dimensional numerical study on influences of uneven equivalence ratio on performances of a rotating detonation combustor
    Liu, Shicheng
    Gao, Chunyu
    Zhou, Shengbing
    [J]. Baozha Yu Chongji/Explosion and Shock Waves, 2024, 44 (05):
  • [10] Numerical study on atomization and evaporation characteristics of preheated kerosene jet in a rotating detonation scramjet combustor
    Wang, Jiasen
    Lin, Wei
    Huang, Weidong
    Shi, Qiang
    Zhao, Jiafeng
    [J]. APPLIED THERMAL ENGINEERING, 2022, 203