Correction to: Characterization of supersonic turbulent combustion in a mach-10 scramjet combustor (aiaa journal)

被引:0
|
作者
Moura, Augusto F. [1 ]
Gibbons, Nicholas [1 ]
Wheatley, Vincent [1 ]
McIntyre, Timothy [1 ]
Jahn, Ingo [1 ]
机构
[1] The University of Queensland, Brisbane,QLD,4072, Australia
来源
AIAA Journal | 2021年 / 59卷 / 04期
关键词
D O I
暂无
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 42 条
  • [1] Characterization of Supersonic Turbulent Combustion in a Mach-10 Scramjet Combustor
    Moura, Augusto F.
    Gibbons, Nicholas
    Wheatley, Vincent
    McIntyre, Timothy
    Jahn, Ingo
    [J]. AIAA JOURNAL, 2020, 58 (05) : 2180 - 2196
  • [2] Characterization of supersonic turbulent combustion in a Mach-10 scramjet combustor
    Moura, Augusto F.
    Gibbons, Nicholas
    Wheatley, Vincent
    McIntyre, Timothy
    Jahn, Ingo
    [J]. AIAA Journal, 2020, 58 (05): : 2180 - 2196
  • [3] Characterization of Supersonic Turbulent Combustion in a Mach-10 Scramjet Combustor (Feb, 10.2514/1.J058671, 2021)
    Moura, Augusto F.
    Gibbons, Nicholas
    Wheatley, Vincent
    McIntyre, Timothy
    Jahn, Ingo
    [J]. AIAA JOURNAL, 2021, 59 (04) : 1 - 1
  • [4] Numerical Simulation of Supersonic Nonpremixed Turbulent Combustion in a Scramjet Combustor Model
    Mura, Arnaud
    Izard, Jean-Francois
    [J]. JOURNAL OF PROPULSION AND POWER, 2010, 26 (04) : 858 - 868
  • [5] Enhanced Supersonic Combustion Targeting Combustor Length Reduction in a Mach 12 Scramjet
    Landsberg, Will O.
    Wheatley, Vincent
    Smart, Michael K.
    Veeraragavan, Ananthanarayanan
    [J]. AIAA JOURNAL, 2018, 56 (10) : 3802 - 3807
  • [6] Enhanced supersonic combustion targeting combustor length reduction in a Mach 12 scramjet
    [J]. 1600, AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States (56):
  • [7] Effects of Oxygen Enrichment on Supersonic Combustion in a Mach 10 Scramjet
    Moura, Augusto F.
    Gibbons, Nicholas
    Wheatley, Vincent
    Jahn, Ingo
    [J]. AIAA JOURNAL, 2021, 59 (11) : 4556 - 4568
  • [8] Effect of boundary layer thickness on supersonic combustion in a scramjet combustor
    Li, Fan
    Zhao, Guoyan
    Huang, Yuhui
    Yang, Daoning
    Ma, Guangwei
    Li, Yansong
    Yang, Yixin
    Li, Peibo
    Zhu, Jiajian
    Sun, Mingbo
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 139
  • [9] Optimization of scramjet inlet based on temperature and Mach number of supersonic combustion
    Araujo, Pedro P. B.
    Pereira, Marcos V. S.
    Marinho, George S.
    Martos, Joao F. A.
    Toro, Paulo G. P.
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 116
  • [10] Combustion enhancement via tandem cavities within a Mach 8 scramjet combustor
    Mecklem, Sarah A.
    Landsberg, Will O.
    Curran, Damian
    Veeraragavan, Ananthanarayanan
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 124