Suppression of Supersonic Cavity Oscillations Using Pulsed Upstream Mass Injection

被引:2
作者
Li, Weipeng [1 ]
机构
[1] Shanghai Jiao Tong Univ, Dept Aeronaut & Astronaut, Shanghai 200240, Peoples R China
基金
中国国家自然科学基金;
关键词
FLOW; LOADS;
D O I
10.1155/2016/6702385
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Pulsed upstream mass injection is examined to suppress supersonic cavity oscillations. The efficiency and physics of the noise control are investigated by large-eddy simulations of a turbulent flow (M-infinity = 2.0, Re-D = 10(5)) past a rectangular cavity with a length-to-depth ratio of 2. Results show that the pulsed mass injection behaves less effectively in reducing the cavity oscillations than the steady one. The primary reason is that the pulsed mass injection is ineffective in lifting up the cavity shear layer and in suppressing the turbulent fluctuations in the shear layer. It concluded that breakup of the large-scale vorticial structures into a smaller length scale reveals direct links existing between the large-scale vortices and the radiation of the cavity resonances.
引用
收藏
页数:6
相关论文
共 40 条
  • [1] Mechanism of controlling supersonic cavity oscillations using upstream mass injection
    Li, Weipeng
    Nonomura, Taku
    Fujii, Kozo
    PHYSICS OF FLUIDS, 2013, 25 (08)
  • [2] Mixing Characteristics in a Supersonic Combustor with Gaseous Fuel Injection Upstream of a Cavity Flameholder
    Sun, Ming-bo
    Geng, Hui
    Liang, Jian-han
    Wang, Zhen-guo
    FLOW TURBULENCE AND COMBUSTION, 2009, 82 (02) : 271 - 286
  • [3] Parametric experimental and numerical study on mixing characteristics in a supersonic combustor with gaseous fuel injection upstream of cavity flameholders
    Sun, M. B.
    Zhang, S. P.
    Han, X.
    Liu, W. D.
    Liang, J. H.
    Wang, Z. G.
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2010, 224 (G5) : 527 - 540
  • [4] Slat Noise Suppression with Mass Injection
    Huang, Hua
    Li, Weipeng
    Wang, Fuxin
    JOURNAL OF AIRCRAFT, 2015, 52 (01): : 31 - 41
  • [5] Supersonic cavity shear layer control using spanwise pulsed spark discharge array
    Kong, Yakang
    Wu, Yun
    Zong, Haohua
    Guo, Shanguang
    PHYSICS OF FLUIDS, 2022, 34 (05)
  • [6] An Analysis of Thrust Vectoring in a Supersonic Nozzle using Bypass Mass Injection
    Islam, Md. Shafiqul
    Hasan, Md. Arafat
    Hasan, A. B. M. Toufique
    PROCEEDINGS OF THE 12TH INTERNATIONAL CONFERENCE ON MECHANICAL ENGINEERING (ICME 2017), 2018, 1980
  • [7] Numerical investigation of mixing enhancement in a cavity-based supersonic combustor using the upstream wavy wall
    Wang, Kaifeng
    Cao, Wei
    INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2025, 114 : 18 - 30
  • [8] Combustion characteristics in a supersonic combustor with ethylene injection upstream of dual parallel cavities
    Zhong, Zhan
    Wang, Zhenguo
    Sun, Mingbo
    Wang, Hongbo
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 230 (13) : 2515 - 2522
  • [9] Cavity Resonance Suppression Using Fluidic Spoilers
    Bennett, Gareth J.
    Okolo, Patrick N.
    Zhao, Kun
    Philo, John
    Guan, Yaoyi
    Morris, Scott C.
    AIAA JOURNAL, 2019, 57 (02) : 706 - 719
  • [10] Experimental investigation on upstream-injection interaction with a scramjet cavity flameholder
    Sun, Ming-Bo
    Zhang, Shun-Ping
    Zhao, Yan-Hui
    Zhao, Yu-Xin
    Liang, Jian-Han
    CHINESE SCIENCE BULLETIN, 2014, 59 (14): : 1568 - 1574