Numerical study of supersonic boundary-layer transition due to sonic wall injection

被引：0
|
作者：
机构：
[1] [1,André, T.
[2] 2,Durant, A.
[3] 1,3,Fedioun, I.
来源：
| 1600年 / AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States卷 / 55期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Dynamic mode decomposition
引用
收藏
相关论文
共 50 条
  • [1] Numerical Study of Supersonic Boundary-Layer Transition due to Sonic Wall Injection
    Andre, T.
    Durant, A.
    Fedioun, I.
    AIAA JOURNAL, 2017, 55 (05) : 1530 - 1547
  • [2] Hypersonic Boundary-Layer Transition Forced by Wall Injection: A Numerical Study
    Orlik, E.
    Fedioun, I.
    Lardjane, N.
    JOURNAL OF SPACECRAFT AND ROCKETS, 2014, 51 (04) : 1306 - 1318
  • [3] NUMERICAL STUDY OF STRONG SLOT INJECTION INTO A SUPERSONIC LAMINAR BOUNDARY-LAYER
    NAPOLITANO, M
    AIAA JOURNAL, 1980, 18 (01) : 72 - 77
  • [4] Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion
    Xue, Rui
    Zheng, Xing
    Yue, Lianjie
    Zhang, Shikong
    Weng, Chao
    ACTA ASTRONAUTICA, 2020, 174 : 11 - 23
  • [5] Wall pressure fluctuation spectra due to boundary-layer transition
    Park, Sewon
    Lauchle, Gerald C.
    JOURNAL OF SOUND AND VIBRATION, 2009, 319 (3-5) : 1067 - 1082
  • [6] SLOT INJECTION INTO A SUPERSONIC LAMINAR BOUNDARY-LAYER
    SMITH, FT
    STEWARTSON, K
    PROCEEDINGS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL AND PHYSICAL SCIENCES, 1973, 332 (1588) : 1 - 22
  • [7] NOTE ON BOUNDARY-LAYER TRANSITION IN SUPERSONIC FLOW
    LANGE, AH
    LEE, RE
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1954, 21 (01): : 58 - 58
  • [8] NUMERICAL EXPERIMENTS IN SUPERSONIC BOUNDARY-LAYER STABILITY
    ERLEBACHER, G
    HUSSAINI, MY
    PHYSICS OF FLUIDS A-FLUID DYNAMICS, 1990, 2 (01): : 94 - 104
  • [9] EXPERIMENTS ON BOUNDARY-LAYER TRANSITION AT SUPERSONIC SPEEDS
    VANDRIEST, ER
    BOISON, JC
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (12): : 885 - 899
  • [10] INITIATION OF BOUNDARY-LAYER TRANSITION IN SUPERSONIC FLOW
    VAUCHERET, X
    RECHERCHE AEROSPATIALE, 1967, (120): : 25 - +
12345