| Literature DB >> 32370255 |
Yasutaka Omori1, Yuki Tamakuma2, Eka Djatnika Nugraha3, Takahito Suzuki4, Miki Arian Saputra3, Masahiro Hosoda2,3, Shinji Tokonami2.
Abstract
Air exchange through a porous medium depends partly on a pressure gradient induced in it, i.e., air-flow conditions of the outer air. Consequently, response of diffusion-type detectors to radon and thoron may vary with air-flow conditions surrounding the detectors. This effect may be significant for thoron measurement because thoron has a shorter half-life than radon. The present study examined response of diffusion-type detectors (RADUETs and one AlphaGUARD) to thoron with respect to wind speed using a thoron calibration chamber. Response of RADUETs to thoron increased with wind speed. Response of the AlphaGUARD increased with wind speed, but it became constant at a high wind speed. Different response trends to thoron between the RADUETs and the AlphaGUARD could be qualitatively explained by flow states induced by the pressure gradient in the filter or the sponge of these detectors. For RADUETs, laminar (Darcy) flow was induced in the sponge in the examined wind speed range, which meant that thoron entry into the detector increased with wind speed. For the AlphaGUARD, laminar flow was induced in the filter in the low wind speed range, whereas flow was changed to turbulent (non-Darcy) flow at a high wind speed for which thoron entry into the detector did not depend on wind speed.Entities:
Keywords: Darcy flow; advection; air exchange; diffusion-type detector; laminar flow; non-Darcy flow; porous medium; radon; thoron; turbulent flow
Year: 2020 PMID: 32370255 PMCID: PMC7246621 DOI: 10.3390/ijerph17093178
Source DB: PubMed Journal: Int J Environ Res Public Health ISSN: 1660-4601 Impact factor: 3.390
Figure 1Views of the detectors examined in the present study: RADUET (a) and AlphaGUARD (b).
Figure 2Schematic representations of the thoron calibration chamber system (a) and experimental setup for exposures of the RADUETs and AlphaGUARD to thoron (b). Panel (a) is modified from Pornnumpa et al. [33].
Wind speed in the thoron calibration chamber at four rotational speed levels of direct current (DC) fans.
| Rotational Speed Level | Wind Speed (m s−1) | ||
|---|---|---|---|
| Center 1 | Near Wall 1 | Average 2 | |
| Very low | 0.33 ± 0.01 | 0.20 ± 0.02 | 0.27 |
| Low | 0.75 ± 0.02 | 0.44 ± 0.03 | 0.59 |
| Reference | 0.85 ± 0.05 | 0.85 ± 0.05 | 0.85 |
| High | 1.84 ± 0.05 | 2.00 ± 0.06 | 1.92 |
1 Average value ± one standard deviation obtained from the repeated measurements. 2 Wind speed averaged at the center and near wall.
Figure 3Examples of temporal variations in thoron concentration in the thoron calibration chamber during exposures of the RADUETs (a) and the AlphaGUARD (b) to thoron. In (b), values indicated by the AlphaGUARD are also shown. Meanings of symbols are the same as those in Equations (3) and (4).
Results of exposure of RADUETs and AlphaGUARD to thoron under variable wind speeds in the thoron calibration chamber.
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| 0.27 | 71 | 1082 | 12.6 ± 1.3 | 0.012 ± 0.001 | |
| 0.59 | 82 | 1281 | 24.6 ± 1.8 | 0.019 ± 0.001 | |
| 0.85 | 72 | 1016 | 19.7 ± 0.5 | 0.019 ± 0.001 | |
| 1.92 | 87 | 1007 | 24.0 ± 0.7 | 0.024 ± 0.001 | |
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| 0.27 | 21 | 12752 ± 359 | 549 ± 42 | 11 ± 3 | 0.042 ± 0.004 |
| 0.59 | 17 | 12294 ± 323 | 816 ± 37 | 11 ± 3 | 0.065 ± 0.003 |
| 0.85 | 16 | 932 ± 80 | 98 ± 12 | 4 ± 2 | 0.101 ± 0.016 |
| 0.85 | 17 | 1049 ± 65 | 89 ± 9 | 8 ± 3 | 0.078 ± 0.011 |
| 0.85 | 20 | 12254 ± 680 | 900 ± 50 | 11 ± 3 | 0.073 ± 0.006 |
| 1.92 | 12 | 1165 ± 76 | 115 ± 13 | 9 ± 3 | 0.091 ± 0.013 |
| 1.92 | 15 | 1014 ± 117 | 94 ± 9 | 10 ± 3 | 0.083 ± 0.013 |
1 Average value ± one standard deviation obtained from five detectors. 2 Average value ± one standard deviation obtained from 12 to 21 datapoints in successive time series.
Figure 4Scatter plots of responses of the RADUETs (a) and the AlphaGUARD (b) to thoron with respect to wind speed in the thoron calibration chamber. Bars on datapoints represent ranges of one standard deviation.
Figure 5Schematic representation of flow regimes in a porous medium. The broken line follows Darcy’s law. This figure is modified from Basak [37] and Macini et al. [40].