Investigation on start performance of scramjet inlet

被引:0
|
作者
Song, Wenyan [1 ]
Ma, Xiaofeng [1 ]
Liu, Weixiong [1 ]
He, Wei [1 ]
机构
[1] School of Power and Energy, Northwestern Polytechnical University, Xi'an 710072
关键词
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
页码:62 / 68
相关论文
共 50 条
  • [41] Experimental investigation of a two-dimensional and a three-dimensional scramjet inlet at Mach 7
    Haeberle, J.
    Guelhan, A.
    JOURNAL OF PROPULSION AND POWER, 2008, 24 (05) : 1023 - 1034
  • [42] Characteristics of the pressure relief slot on the start performance of the hypersonic inlet
    Zhong, Jiaxiang
    Qu, Feng
    Wang, Qing
    PHYSICS OF FLUIDS, 2025, 37 (03)
  • [43] Design and analysis of thermal structure of inlet of scramjet
    School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
    Hangkong Dongli Xuebao, 2008, 11 (1961-1965):
  • [44] INVISCID ANALYSIS OF A DUAL MODE SCRAMJET INLET
    HSIA, YC
    GROSS, BJ
    ORTWERTH, JP
    JOURNAL OF PROPULSION AND POWER, 1991, 7 (06) : 1030 - 1035
  • [45] Unsteady pressure behavior in a Ramjet/Scramjet inlet
    Rodi, PE
    Emami, S
    Trexler, CA
    JOURNAL OF PROPULSION AND POWER, 1996, 12 (03) : 486 - 493
  • [46] Interaction of shock/boundary layers in a scramjet inlet
    Wang, Ge
    Jiang, Xu-Xu
    Tang, Qiang
    Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University, 2007, 28 (11): : 1206 - 1212
  • [47] Numerical Investigation into the Combustion Behavior of an Inlet-Fueled Thermal-Compression-Like Scramjet
    Bricalli, Mathew G.
    Brown, Laurie M.
    Boyce, Russell R.
    AIAA JOURNAL, 2015, 53 (07) : 1740 - 1760
  • [48] Investigation of a variable geometry scramjet inlet with a rotating cowl operating in a large Mach number range
    Jin, Zhi-Guang
    Zhang, Kun-Yuan
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2010, 25 (07): : 1553 - 1560
  • [49] Investigation on Unstart/Start Phenomenon of Supersonic Inlet Caused by Back Pressure
    Zhao H.
    Xie L.-R.
    Ge Y.
    Huang K.-W.
    Zeng Q.
    Tuijin Jishu/Journal of Propulsion Technology, 2020, 41 (10): : 2204 - 2212
  • [50] Computational investigation to study the effect of a hybrid hydrogen fuelled scramjet combustor on different inlet boundary conditions
    Bordoloi, Namrata
    Pandey, K. M.
    Sharma, K. K.
    MATERIALS TODAY-PROCEEDINGS, 2021, 45 : 6774 - 6782