On mixing enhancement via nozzle trailing-edge modifications in high-speed jets

被引：0
|
作者：
机构：
[1] Kim, J.-H.
[2] Samimy, M.
来源：
Kim, J.-H. | 1600年 / AIAA, United States卷 / 38期
关键词：
Theoretical; (THR);
D O I：
暂无
中图分类号：
学科分类号：
摘要：
This study demonstrates that a cutout on the contoured nozzle block is effective in mixing enhancement in all flow regimes, including the ideally expanded regime. It is shown that the role of streamwise vortices in the jet development of the ideally expanded case is similar to those in the underexpanded case.
引用
收藏
相关论文
共 50 条
  • [41] Influence of blade trailing edge profile on pressure pulsation in high-speed centrifugal pump
    Cui, Baoling
    Chen, Zhanyun
    Zhang, Yingbin
    AIP ADVANCES, 2024, 14 (06)
  • [42] Lift enhancement and flow structure of airfoil with joint trailing-edge flap and Gurney flap
    Lee, T.
    Su, Y. Y.
    EXPERIMENTS IN FLUIDS, 2011, 50 (06) : 1671 - 1684
  • [43] Trailing edge loss analysis of high-speed cryogenic microturbines used in helium applications
    Sam, Ashish Alex
    Ghosh, Parthasarathi
    CRYOGENICS, 2020, 106
  • [44] Supersonic jet noise control via trailing edge modifications
    Kim, JH
    Lee, S
    KSME INTERNATIONAL JOURNAL, 2001, 15 (08): : 1174 - 1180
  • [45] A study on trailing edge noise sources using high-speed particle image velocimetry
    Schroeder, A.
    Herr, M.
    Lauke, T.
    Dierksheide, U.
    NEW RESULTS IN NUMERICAL AND EXPERIMENTAL FLUID MECHANICS V, 2006, 92 : 373 - +
  • [46] Supersonic jet noise control via trailing edge modifications
    Jin-Hwa Kim
    Seungbae Lee
    KSME International Journal, 2001, 15 : 1174 - 1180
  • [47] GENERATION OF HIGH-SPEED LIQUID JETS BY HIGH-SPEED IMPACT OF A PROJECTILE
    SHI, HH
    TAKAYAMA, K
    JSME INTERNATIONAL JOURNAL SERIES B-FLUIDS AND THERMAL ENGINEERING, 1995, 38 (02): : 181 - 190
  • [48] EXPERIMENTAL RESULTS ON EDGE-TONE OSCILLATIONS IN HIGH-SPEED SUBSONIC JETS
    LEPICOVSKY, J
    AHUJA, KK
    AIAA JOURNAL, 1985, 23 (10) : 1463 - 1468
  • [49] Analysis of a Wing-Fuselage Biplane with Trailing-Edge Flaps in Low-Speed Flow
    Duong Nguyen, Thai
    Kashitani, Masashi
    Kusunose, Kazuhiro
    Taguchi, Masato
    Takita, Yoshihiro
    JOURNAL OF AIRCRAFT, 2022, 59 (02): : 350 - 363
  • [50] Investigation of noise sources in high-speed jets via correlation measurements
    Panda, J
    Seasholtz, RG
    Elam, KA
    JOURNAL OF FLUID MECHANICS, 2005, 537 : 349 - 385
12345