Experimental investigation of the turbulent Schmidt number in supersonic film cooling with shock interaction

被引:0
|
作者
Pascal Marquardt
Michael Klaas
Wolfgang Schröder
机构
[1] Chair of Fluid Mechanics and Institute of Aerodynamics Aachen,
来源
Experiments in Fluids | 2020年 / 61卷
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] Effects of shock wave impingement on supersonic film cooling
    Takita, Kenichi
    Masuya, Goro
    Journal of Spacecraft and Rockets, 36 (04): : 602 - 604
  • [22] Experimental and numerical study of supersonic film cooling
    Aupoix, B
    Mignosi, A
    Viala, S
    Bouvier, F
    Gaillard, R
    AIAA JOURNAL, 1998, 36 (06) : 915 - 923
  • [23] Experimental investigation of influence of Reynolds number on supersonic film aero-optics
    College of Aerospace Science and Engineering, National University of Defense Technology, Changsha
    410073, China
    Hongwai yu Jiguang Gongcheng Infrared Laser Eng., 2
  • [24] FLOWFIELD MEASUREMENTS IN SUPERSONIC FILM-COOLING INCLUDING THE EFFECT OF SHOCK-WAVE INTERACTION
    JUHANY, KA
    HUNT, ML
    AIAA JOURNAL, 1994, 32 (03) : 578 - 585
  • [25] Investigation of shock wave influence on supersonic transpiration cooling
    Jiang, Pei-Xue (jiangpx@mail.tsinghua.edu.cn), 1600, Science Press (35):
  • [26] Experimental investigation of shock/vortex interaction for slender canard configurations at supersonic speed
    Leopold, F
    Jagusinski, F
    Demeautis, C
    ICIASF'03 RECORD: 20TH INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES, 2003, : 247 - 257
  • [27] Study of a supersonic reacting wall jet with a variable turbulent Prandtl and Schmidt number approach
    Hoste, J. J. O. E.
    Fechter, S.
    Karl, S.
    Hannemann, K.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 106
  • [28] Influence of shock wave impinging region on supersonic film cooling
    Xiaokai SUN
    Hang NI
    Wei PENG
    Peixue JIANG
    Yinhai ZHU
    Chinese Journal of Aeronautics, 2021, 34 (05) : 452 - 465
  • [29] Effect of shock waves on supersonic film cooling with a slotted wall
    Peng, Wei
    Jiang, Pei-Xue
    APPLIED THERMAL ENGINEERING, 2014, 62 (01) : 187 - 196
  • [30] Influence of shock wave impinging region on supersonic film cooling
    Xiaokai SUN
    Hang NI
    Wei PENG
    Peixue JIANG
    Yinhai ZHU
    Chinese Journal of Aeronautics , 2021, (05) : 452 - 465