Abstract
AbstractThis 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 [$$768 \times 924$$
768
×
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 $$300\, \upmu \hbox {sec}$$
300
μ
sec
and to track evolveness over a distance of 100 mm. Our findings show that processing of high-speed videos can enrich, and give detailed insight, to the observations in the shock experiments.
Funder
University Of South-Eastern Norway
Publisher
Springer Science and Business Media LLC
Subject
Electrical and Electronic Engineering,Signal Processing
Reference16 articles.
1. Settle, G.S., Hargather, M.H.: A review of recent developments in schlieren and shadowgraph techniques. Meas. Sci. Technol. 28, 042001 (2017). https://doi.org/10.1088/1361-6501/AA5748
2. Damazo, J.S.: Planar Reflection of Gaseous Detonations. Doctoral Thesis, California Institute of Technology, Pasadena, California (2013)
3. Timmerman, B.H., Skeen, A.J., Bryanston-Cross, P.J., Tucker, P.G., Jefferson-Loveday, R.J., Paduano, J.D., Guenette, G.R.: High-speed digital visualization and high-frequency automated shock tracking in supersonic lows. Opt. Eng. 48, 10 (2008). https://doi.org/10.1117/1.2992621
4. Mark, H.: The Interaction of a Reflected Shock Wave With the Boundary layer in a shock tube. Cornell University, Ithaca, New York (1958)
5. Babinsky, H., Harvey, J.K.: Shock Wave-Boundary-Layer Interactions. Cambridge University Press, London (2012). https://doi.org/10.1017/CBO9780511842757
Cited by
3 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献