Numerical simulation of axial liquid film cooling in rocket combustor

被引:0
|
作者
School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100191, China [1 ]
机构
来源
Hangkong Dongli Xuebao | 2013年 / 2卷 / 459-465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 50 条
  • [21] Numerical simulation of blown film cooling
    Sidiropoulos, V
    Vlachopoulos, J
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2002, 21 (07) : 629 - 637
  • [22] Numerical simulation of blown film cooling
    Sidiropoulos, V
    Vlachopoulos, J
    ANTEC 2000: SOCIETY OF PLASTICS ENGINEERS TECHNICAL PAPERS, CONFERENCE PROCEEDINGS, VOLS I-III, 2000, : 312 - 315
  • [23] Numerical analysis of regenerative cooling in liquid propellant rocket engines
    Ulas, A.
    Boysan, E.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2013, 24 (01) : 187 - 197
  • [24] Numerical Investigation of Gas Turbine Combustor Liner Film Cooling Slots
    Kiyici, Firat
    Topal, Ahmet
    Hepkaya, Ender
    Inanli, Sinan
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 5C, 2018, : 43 - 52
  • [25] NUMERICAL STUDY OF FILM COOLING ENHANCEMENT IN GAS TURBINE COMBUSTOR LINER
    Subbuswamy, Ganesh
    Li, Xianchang
    IMECE 2008: HEAT TRANSFER, FLUID FLOWS, AND THERMAL SYSTEMS, VOL 10, PTS A-C, 2009, : 1237 - 1247
  • [26] Supervised learning mixing characteristics of film cooling in a rocket combustor using convolutional neural networks
    Ma, Hao
    Zhang, Yu-xuan
    Haidn, Oskar J.
    Thuerey, Nils
    Hu, Xiang-yu
    ACTA ASTRONAUTICA, 2020, 175 : 11 - 18
  • [27] A new generalised model for liquid film cooling in rocket combustion chambers
    Shine, S. R.
    Kumar, S. Sunil
    Suresh, B. N.
    INTERNATIONAL JOURNAL OF HEAT AND MASS TRANSFER, 2012, 55 (19-20) : 5065 - 5075
  • [28] Establishment of Design Method for Liquid Hydrogen Regenerative Cooling Combustor of LOX/Hydrogen Rocket Engine
    Yatsuyanagi, Nobuyuki
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2009, 51 (174) : 259 - 266
  • [29] Establishment of design method for liquid hydrogen regenerative cooling combustor of LOX/hydrogen rocket engine
    Yatsuyanagi, Nobuyuki
    Transactions of the Japan Society for Aeronautical and Space Sciences, 2008, 51 (174): : 259 - 266
  • [30] Test and simulation of film cooling length in conventional propellant rocket engine
    Hou R.
    Chen J.
    Li L.
    Yang J.
    Zhang G.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2023, 38 (11): : 2799 - 2808