Processing of high-speed videos of shock wave boundary layer interactions

被引:3
|
作者
Maharjan, Samee [1 ]
Bjerketvedt, Dag [1 ]
Lysaker, Ola Marius [1 ]
机构
[1] Univ South Eastern Norway, Kjolnes Ring 56, N-3918 Porsgrunn, Norway
关键词
Image processing; Front tracking; Shock wave; High-speed videos;
D O I
10.1007/s11760-020-01782-5
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
This paper presents a framework for processing high-speed videos recorded during gas experiments in a shock tube. The main objective is to study boundary layer interactions of reflected shock waves in an automated way, based on image processing. The shock wave propagation was recorded at a frame rate of 500,000 frames per second with a Kirana high-speed camera. Each high-speed video consists of 180 frames, with image size [768 x 924] pixels. An image processing framework was designed to track the wave front in each image and thereby estimate: (a) the shock position; (b) position of triple point; and (c) shock angle. The estimated shock position and shock angle were then used as input for calculating the pressure exerted by the shock. To validate our results, the calculated pressure was compared with recordings from pressure transducers. With the proposed framework, we were able to identify and study shock wave properties that occurred within less than 300 mu sec and to track evolveness over a distance of 100mm. Our findings show that processing of high-speed videos can enrich, and give detailed insight, to the observations in the shock experiments.
引用
收藏
页码:607 / 615
页数:9
相关论文
共 50 条
  • [21] Interactions between oblique second mode and oblique waves in a high-speed boundary layer
    Zhou, Teng
    Liu, Zaijie
    Lu, Yuhan
    Yan, Chao
    JOURNAL OF FLUID MECHANICS, 2023, 973
  • [22] RAINDROP BREAKUP IN SHOCK LAYER OF A HIGH-SPEED VEHICLE
    WALDMAN, GD
    GLENN, DC
    REINECKE, WG
    AIAA JOURNAL, 1972, 10 (09) : 1200 - &
  • [23] Shock-wave/boundary layer interactions at hypersonic speed by an implicit Navier-Stokes solver
    Leyland, P
    INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, 1996, 6 (01) : 71 - 87
  • [24] A computational investigation of laminar shock/wave boundary layer interactions
    Deepak, N.R. (deepak.narayan@gmail.com), 1600, Royal Aeronautical Society (117):
  • [25] Crossflow effects on shock wave/turbulent boundary layer interactions
    Mario Di Renzo
    Nikhil Oberoi
    Johan Larsson
    Sergio Pirozzoli
    Theoretical and Computational Fluid Dynamics, 2022, 36 : 327 - 344
  • [26] Effects of Herringbone Riblets on Shock Wave Boundary Layer Interactions
    Wang G.
    Wen B.
    Zhang K.-L.
    Yang Y.-G.
    Yuhang Xuebao/Journal of Astronautics, 2020, 41 (01): : 27 - 34
  • [27] Some physical aspects of shock wave/boundary layer interactions
    Jean Délery
    Jean-Paul Dussauge
    Shock Waves, 2009, 19 : 453 - 468
  • [28] A computational investigation of laminar shock/wave boundary layer interactions
    Deepak, N. R.
    Gai, S. L.
    Neely, A. J.
    AERONAUTICAL JOURNAL, 2013, 117 (1187): : 27 - 56
  • [29] Crossflow effects on shock wave/turbulent boundary layer interactions
    Di Renzo, Mario
    Oberoi, Nikhil
    Larsson, Johan
    Pirozzoli, Sergio
    THEORETICAL AND COMPUTATIONAL FLUID DYNAMICS, 2022, 36 (02) : 327 - 344
  • [30] Passive control of shock wave-boundary-layer interactions
    Gibson, TM
    Babinsky, H
    Squire, LC
    AERONAUTICAL JOURNAL, 2000, 104 (1033): : 129 - 140