EFFECT OF THE BOUNDARY LAYER UPON THE FLOW IN A CONICAL HYPERSONIC NOZZLE

被引：2
|
作者：
SICHEL, M
机构：
来源：
AIAA JOURNAL | 1964年 / 2卷 / 01期
关键词：
D O I：
10.2514/3.2269
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：180 / 183
页数：4
相关论文
共 50 条
  • [1] Effect of wall microstructure on conical hypersonic boundary layer flow
    Zhang, Zhen
    Yi, Shihe
    Liu, Xiaolin
    Hu, Yufa
    PHYSICS OF FLUIDS, 2024, 36 (10)
  • [2] INVESTIGATION OF BOUNDARY-LAYER SEPARATION IN A HYPERSONIC CONICAL NOZZLE.
    Gorenbukh, P.I.
    Fluid mechanics. Soviet research, 1979, 8 (01): : 9 - 16
  • [3] BOUNDARY LAYER IN HYPERSONIC FLOW
    HILL, FK
    PHYSICAL REVIEW, 1953, 91 (04): : 1029 - 1030
  • [4] Hypersonic nozzle-afterbody experiment: Flow visualization and boundary-layer measurements
    Keener, ER
    Spaid, FW
    JOURNAL OF SPACECRAFT AND ROCKETS, 1996, 33 (03) : 326 - 332
  • [5] HYPERSONIC CONICAL FLOW
    WILLIAMS, H
    ARS JOURNAL, 1959, 29 (09): : 668 - 670
  • [6] Influence of disturbances generated by the nozzle boundary layer on the heat exchange on the cylindrical nose of a body in a hypersonic flow
    Bezmenov V.Ya.
    Borovoy V.Ya.
    Struminskaya I.V.
    Yakovleva L.V.
    Fluid Dynamics, 1999, 34 (1) : 105 - 109
  • [7] Experimental investigations of disturbance development in the hypersonic boundary layer on a conical model
    Bountin, DA
    Shiplyuk, AN
    Sidorenko, AA
    LAMINAR-TURBULENT TRANSITION, 2000, : 475 - 480
  • [8] BOUNDARY-LAYER MEASUREMENTS IN HYPERSONIC FLOW
    HILL, FK
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (01): : 35 - 42
  • [9] Modeling flow transition in hypersonic boundary layer
    Fu, S.
    Wang, L.
    NEW TRENDS IN FLUID MECHANICS RESEARCH: PROCEEDINGS OF THE FIFTH INTERNATIONAL CONFERENCE ON FLUID MECHANICS, 2007, : 53 - 56
  • [10] ON THE BOUNDARY-LAYER EQUATIONS IN HYPERSONIC FLOW
    SHEN, SF
    JOURNAL OF THE AERONAUTICAL SCIENCES, 1952, 19 (07): : 500 - 501
12345