EXPERIMENTAL INVESTIGATIONS OF AN UNDEREXPANDED JET FROM A CONVERGENT NOZZLE IMPINGING ON A CAVITY

被引：18
|
作者：
SOBIERAJ, GB
SZUMOWSKI, AP
机构：
[1] Technical University, 00-665 Warszawa
来源：
JOURNAL OF SOUND AND VIBRATION | 1991年 / 149卷 / 03期
关键词：
D O I：
10.1016/0022-460X(91)90443-N
中图分类号：
O42 [声学];
学科分类号：
070206 ; 082403 ;
摘要：
The influence of the detailed shape of the nozzle exit and the cavity inlet edge on the oscillating flow characteristics are investigated. The experiments show that the shape of the cavity edge considerably influences acoustical and thermal effects as well as the oscillatory mode (screech and regurgitant) switching. The shape of the nozzle exit edge has a minor significance. The screech oscillation mode mechanism and some details of the regurgitant mode are determined from external flow visualization and pressure measurements. Some characteristics of the near flow field induced by an oscillating jet are also obtained. © 1991.
引用
收藏
页码：375 / 396
页数：22
相关论文
共 50 条
  • [1] Study on underexpanded impinging jet issued from rectangular nozzle
    Azam, Ruhul
    Ozono, Hiroaki
    Yaga, Minoru
    Teruya, Isao
    Ishikawa, Masaaki
    [J]. 5TH BSME INTERNATIONAL CONFERENCE ON THERMAL ENGINEERING, 2013, 56 : 269 - 274
  • [2] Characteristics of Underexpanded Supersonic Impinging Jet Caused by Rectangular Nozzle
    Yasunobu, Tsuyoshi
    Jiang, Xin
    Komatani, Kairi
    Fujiwara, Yuta
    [J]. RECENT ASIAN RESEARCH ON THERMAL AND FLUID SCIENCES, AJWTF7 2018, 2020, : 125 - 132
  • [3] JET EMERGING FROM A NOZZLE AND IMPINGING ON A CONICAL CAVITY: INFLUENCE OF NOZZLE AND CAVITY GEOMETRIC CONFIGURATIONS
    Shuja, S. Z.
    Yilbas, B. S.
    [J]. NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2012, 61 (02) : 142 - 162
  • [4] AN EXPERIMENTAL-STUDY ON AN UNDEREXPANDED ANNULAR IMPINGING JET
    MASUDA, W
    NAKAMURA, T
    KOBAYASHI, M
    SAITO, H
    [J]. JSME INTERNATIONAL JOURNAL SERIES II-FLUIDS ENGINEERING HEAT TRANSFER POWER COMBUSTION THERMOPHYSICAL PROPERTIES, 1990, 33 (04): : 674 - 679
  • [5] Nozzle external geometry as a boundary condition for the azimuthal mode selection in an impinging underexpanded jet
    Weightman, Joel L.
    Amili, Omid
    Honnery, Damon
    Edgington-Mitchell, Daniel
    Soria, Julio
    [J]. JOURNAL OF FLUID MECHANICS, 2019, 862 : 421 - 448
  • [6] Behavior of underexpanded jet impinging on sphere
    Endo, Masaki
    Sakakibara, Yoko
    Iwamoto, Junjiro
    [J]. FEDSM 2007: PROCEEDINGS OF THE 5TH JOINT AMSE/JSME FLUIDS ENGINEERING SUMMER CONFERENCE VOL 1, PTS A AND B, 2007, : 1671 - 1678
  • [7] Experimental Characterization and Control of an Impinging Jet Issued from a Rocket Nozzle
    Mehta, Yogesh
    Bhargav, Vikas N.
    Kumar, Rajan
    [J]. NEW SPACE-THE JOURNAL OF SPACE ENTREPRENEURSHIP AND INNOVATION, 2021, 9 (03): : 187 - 201
  • [8] Numerical simulation of a low-swirl impinging jet with a rotating convergent nozzle
    Borynyak, K.
    Hrebtov, M.
    Bobrov, M.
    Kozyulin, N.
    [J]. 6TH INTERNATIONAL CONFERENCE HEAT AND MASS TRANSFER AND HYDRODYNAMICS IN SWIRLING FLOWS, 2018, 980
  • [9] FLOWFIELD OF A HIGHLY UNDEREXPANDED JET IMPINGING ON A SURFACE
    EASTMAN, DW
    BONNEMA, JP
    [J]. AIAA JOURNAL, 1966, 4 (07) : 1302 - &
  • [10] Flow features of underexpanded microjets emerging from a round convergent nozzle
    Tashiro, Tenta
    Fukunaga, Ryota
    Utsunomiya, Daisuke
    Nakao, Shinichiro
    Miyazato, Yoshiaki
    Ishino, Yojiro
    [J]. EXPERIMENTS IN FLUIDS, 2023, 64 (03)
12345