4.7 Article

Temporally and spatially resolved X-ray densitometry in a shock tube

期刊

COMBUSTION AND FLAME
卷 224, 期 -, 页码 136-149

出版社

ELSEVIER SCIENCE INC
DOI: 10.1016/j.combustflame.2020.09.035

关键词

X-ray absorption; Abel inversion; Tomographic reconstruction; Shock waves; Shock tube; Boundary layer

资金

  1. U.S. Department of Energy, Office of Sciences, Office of Basic Energy Sciences [DE-AC02-06CH11357]
  2. NSF [1747774]
  3. Division of Chemical Sciences, Geosciences, and Biosciences, the Office of Basic Energy Sciences, the U.S. Department of Energy as part of the Argonne Sandia Consortium on High Pressure Combustion Chemistry [DE-AC02-2006CH11357]
  4. Div Of Chem, Bioeng, Env, & Transp Sys
  5. Directorate For Engineering [1747774] Funding Source: National Science Foundation

向作者/读者索取更多资源

Gas densities behind incident and reflected shock waves were measured using x-ray absorption spectroscopy, revealing significant differences in densities as distance from the endwall increased. Abel inversion reconstruction allowed for time and radially resolved densities to be obtained, showing the presence of sidewall thermal boundary layers behind the reflected shock.
Gas densities were measured by x-ray absorption spectroscopy to examine spatial inhomogeneity in density behind incident and reflected shock waves in a miniature (12.7 mm bore) high repetition rate shock tube. Shock waves were generated in argon. The pressure and temperature behind the incident shock were P-2 similar to 1.72 bar and T-2 similar to 800 K, while those behind the reflected shock were P-5 similar to 6.5 bar and T-5 similar to 1480 K. Time-resolved line-of-sight transmission measurements using x-rays at 9 keV photon energy were made along various axial and transverse locations covering the entire shock tube cross section. The x-ray transmission at each location was converted to pathlength-integrated densities, which in some conditions could be further converted to pathlength-averaged densities. The measured gas densities were compared with those calculated by the normal shock wave relations, and good agreement was found in the preshock and immediately behind the incident shock regions. Similar agreement was found for reflected shock conditions very near the endwall. However, increasingly large differences between the measured and calculated gas densities were found as distance from the endwall increased. Reconstruction by Abel inversion allowed time and radially resolved densities to be obtained from the transverse measurements. While the profiles measured in this experiment are of insufficient signal-to noise level and resolution to definitively assign boundary layer thicknesses, future improvements may be able to do this. The radially resolved densities reveal growing sidewall thermal boundary layers in gases behind the reflected shock. These reconstructions were compared with a model of the thermal boundary layer and are consistent with values of the thermal boundary layer thickness being between 0.25 mm and 1 mm at 0.7 ms after shock reflection. (C) 2020 The Combustion Institute. Published by Elsevier Inc. All rights reserved.

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