Oscillatory characteristics of cavities in supersonic flow

被引:2
|
作者
Prasath, M. [1 ,2 ]
Desikan, S. L. N. [1 ]
Vaidyanathan, Aravind [2 ]
机构
[1] Vikram Sarabhai Space Ctr, Thiruvananthapuram, Kerala, India
[2] Indian Inst Space Sci & Technol, Thiruvananthapuram, Kerala, India
关键词
Time-resolved images; Statistical analyses; Fluid-dynamic and fluid-resonant; oscillations; Modal analyses; PROPER ORTHOGONAL DECOMPOSITION; COMPRESSIBLE FLOW; WAVELET TRANSFORM; LAYER;
D O I
10.1016/j.euromechflu.2022.12.005
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
We examine the flow structures, acoustic emissions, and oscillation types for supersonic flow past a baseline cavity and cavity with a bump. To study these, time-resolved shadowgraph images and unsteady pressure measurements are used. According to the results, the baseline cavity oscillates at various dominant frequencies. By adding a bump inside the cavity, many of its dominant oscillations are inactivated which are also corroborated by cross-correlation. Using time-resolved images, we can show the differences in wave propagation mechanisms between the two cavities. Through pressure spectra, it is demonstrated that the baseline cavity displays both fluid-dynamic and fluid-resonant types of oscillations, while the cavity with bump undergoes only the fluid-resonant type. The Rossiter prediction for the baseline cavity is very accurate but greatly deviates when applied to the cavity with a bump. As well, the wavelet analysis reveals that only the baseline cavity undergoes mode-switching phenomena. Additionally, the shear layer large-scale structures influencing the cavity oscillations are identified by using proper orthogonal decomposition (POD) and spectral proper orthogonal decomposition (SPOD) techniques. Furthermore, an analogy is established between POD and SPOD mode shapes along with the shadowgraph images for dominant modes of cavity oscillation. Finally, the results demonstrate that these modal decomposition techniques complement each other.& COPY; 2022 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码:224 / 237
页数:14
相关论文
共 50 条
  • [21] Flow Characteristics of a Supersonic Open Cavity
    J. M. Wang
    X. J. Ming
    H. Wang
    Y. Ma
    J. Q. Wu
    Fluid Dynamics, 2019, 54 : 724 - 738
  • [22] Flow Characteristics of a Supersonic Open Cavity
    Wang, J. M.
    Ming, X. J.
    Wang, H.
    Ma, Y.
    Wu, J. Q.
    FLUID DYNAMICS, 2019, 54 (05) : 724 - 738
  • [23] Supersonic flow characteristics in laser grooving
    Mai, CC
    Lin, JM
    OPTICS AND LASER TECHNOLOGY, 2003, 35 (08): : 597 - 604
  • [24] Experimental investigation on ignition schemes of partially covered cavities in a supersonic flow
    Cai, Zun
    Sun, Mingbo
    Wang, Hongbo
    Wang, Zhenguo
    ACTA ASTRONAUTICA, 2016, 121 : 88 - 94
  • [25] Drag force investigation of cavities with different geometric configurations in supersonic flow
    LUO ShiBin1
    2 Centre for CFD
    Science China(Technological Sciences), 2011, (05) : 1345 - 1350
  • [26] EXPERIMENTAL INVESTIGATION OF SUPERSONIC-FLOW OVER 2 CAVITIES IN TANDEM
    ZHANG, X
    EDWARDS, JA
    AIAA JOURNAL, 1992, 30 (05) : 1182 - 1190
  • [27] HEAT TRANSFER AND DYNAMICS OF SUPERSONIC AIR FLOW PAST CAVITIES.
    VARFOLOMEYEV, I.M.
    GORTYSHEV, YU.F.
    SHCHUKIN, V.K.
    1981, V 13 (N 4): : 86 - 91
  • [28] Drag force investigation of cavities with different geometric configurations in supersonic flow
    Luo ShiBin
    Huang Wei
    Liu Jun
    Wang ZhenGuo
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2011, 54 (05) : 1345 - 1350
  • [29] Drag force investigation of cavities with different geometric configurations in supersonic flow
    LUO ShiBin HUANG Wei LIU Jun WANG ZhenGuo Center of Hypersonic Propulsion Institute of Aerospace and Materials Engineering National University of Defense Technology Changsha China Centre for CFD School of Process Environmental and Materials Engineering University of Leeds LS JT UK
    Science China(Technological Sciences), 2011, 54 (05) : 1345 - 1350