Characteristics of a central bleed jet in supersonic axisymmetric base flow

被引:2
|
作者
Kuehner, Joel P. [1 ]
Anderson, Blake B.
Flittner, Jonathan G.
Dutton, J. Craig
机构
[1] Washington & Lee Univ, Phys & Engn Dept, Lexington, VA 24450 USA
[2] Univ Texas, Dept Mech & Aerosp Engn, Arlington, TX 76019 USA
关键词
D O I
10.2514/1.24838
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The near-wake flow structure of a supersonic axisymmetric base flow with base bleed is investigated in detail using acetone planar laser-induced fluorescence. Global side-view and end-view images are analyzed to detect unstirred bleed fluid, which has been found to persist from the bleed orifice through reattachment (i.e., rear stagnation point). The characteristic size, shape, and location of the bleed fluid pockets are studied. This enables a comparison of the bleed jet structure for three different cases of mass flow rate of bleed fluid. In addition, the average location of the forward stagnation point and the primary and secondary recirculation regions are linked to the distributions of several statistics. The similarities and differences between two suboptimal bleed rate cases identify possible optimal locations for the central bleed jet to be directed. A stabilizing effect caused by increasing bleed rate is documented in many of the statistical quantities. Agreement between side-view and end-view image analysis confirms the ability of the processing technique to distinguish the unstirred bleed fluid in all images.
引用
收藏
页码:347 / 354
页数:8
相关论文
共 50 条
  • [21] Numerical simulation of base flow with hot base bleed for two jet models
    Yu, Wen-Jie
    Yu, Yong-Gang
    Ni, Bin
    DEFENCE TECHNOLOGY, 2014, 10 (03): : 279 - 284
  • [22] Base Flow and Drag Characteristics of a Supersonic Vehicle with Cold and Hot Jet Flows of Nozzles
    Kim, Yongchan
    Nam, Junyeop
    Roh, Tae-Seong
    Lee, Hyoung Jin
    AEROSPACE, 2023, 10 (10)
  • [23] SUPERSONIC AXISYMMETRIC FLOW OVER BOATTAILS CONTAINING A CENTERED PROPULSIVE JET
    DEIWERT, GS
    AIAA JOURNAL, 1984, 22 (10) : 1358 - 1365
  • [24] Effect of Axisymmetric Sonic Nozzle Geometry on Characteristics of Supersonic Air Jet
    Shigeru MATSUO
    Masanori TANAKA
    Yumiko OTOBE
    Hideo KASHIMURA
    Heuy-Dong KIM
    Toshiaki SETOGUCHI
    JournalofThermalScience, 2004, (02) : 121 - 126
  • [25] Effect of Axisymmetric Sonic Nozzle Geometry on Characteristics of Supersonic Air Jet
    Matsuo, Shigeru
    Tanaka, Masanori
    Otobe, Yumiko
    Kashimura, Hideo
    Kim, Heuy-Dong
    Setoguchi, Toshiaki
    JOURNAL OF THERMAL SCIENCE, 2004, 13 (02) : 121 - 126
  • [26] Effect of axisymmetric sonic nozzle geometry on characteristics of supersonic air jet
    Shigeru Matsuo
    Masanori Tanaka
    Yumiko Otobe
    Hideo Kashimura
    Heuy-Dong Kim
    Toshiaki Setoguchi
    Journal of Thermal Science, 2004, 13 : 121 - 126
  • [27] Experimental investigation of base pressure with hot supersonic jet for external supersonic flow
    Zapryagaev, VI
    Lokotko, AV
    Nikiforov, SV
    Pavlov, AA
    Tchernyshev, AV
    Bannink, WJ
    Ottens, H
    Muylaert, J
    4TH EUROPEAN SYMPOSIUM ON AEROTHERMODYNAMICS FOR SPACE VEHICLES, PROCEEDINGS, 2002, 487 : 579 - 584
  • [28] An investigation on bleed flow control of an axisymmetric supersonic intake based on parametric outline optimization design
    Xie, Peimin
    Liu, Yuanhua
    Yuan, Wei
    AEROSPACE SCIENCE AND TECHNOLOGY, 2025, 159
  • [29] Prediction of the Supersonic Flow Base Pressure by Axisymmetric Direct Numerical Simulation
    Karskanov, S. A.
    Karpov, A. I.
    Shaklein, A. A.
    Lipanov, A. M.
    Rusyak, I. G.
    Korolev, S. A.
    JOURNAL OF APPLIED AND COMPUTATIONAL MECHANICS, 2023, 9 (03): : 739 - 748
  • [30] TURBULENT BASE FLOW ON AN AXISYMMETRIC BODY WITH A SINGLE EXHAUST JET
    DIXON, RJ
    RICHARDSON, JM
    PAGE, RH
    JOURNAL OF SPACECRAFT AND ROCKETS, 1970, 7 (07) : 848 - +