Please use this identifier to cite or link to this item:
Title: Discussion on heat lost through solid boundaries in modeling atrium fires under mechanical exhaust
Authors: Chow, WK 
Yi, L
Shi, CL
Li, YZ
Huo, R
Keywords: Mechanical exhaust
Smoke layer temperature
Heat lost to solid boundaries
Issue Date: 2015
Publisher: Springer
Source: In K Harada, K Matsuyama, K Himoto, Y Nakamura & K Wakatsuki (Eds.), Fire Science and Technology 2015 : The Proceedings of 10th Asia-Oceania Symposium on Fire Science and Technology, p. 105-109. Singapore Springer Singapore, 2017 How to cite?
Abstract: Mechanical smoke exhaust systems are usually required in large atria in the Far East. Systems are designed based on empirical expressions in the literature. Most of those design equations were derived from a two-layer zone modelling approach under some geometrical restrictions. Full-scale burning tests on mechanical smoke exhaust system were carried out. From these experiments, it was found that there are significant differences between the measured results in some of the tests and those calculated from the design equations using a two-layer approach. Mass exchange through the smoke layer and cool air layer was identified earlier to be a key point under some conditions. But heat lost through the solid boundaries is another factor as pointed out recently. This point will be further discussed in this paper. A simple model based on a two-layer approach reported earlier will be applied to justify those design equations and experimental results. © Springer 2015. Selection and peer-review under responsibility of the Asia-Oceania Association for Fire Science and Technology.
Description: 10th Asia-Oceania Symposium on Fire Science and Technology (AOSFST 2015), Tsukuba, Japan, 5-7 October 2015
ISBN: 978-981-10-0375-2 (print)
DOI: 10.1007/978-981-10-0376-9_10
Appears in Collections:Conference Paper

View full-text via PolyU eLinks SFX Query
Show full item record

Page view(s)

Last Week
Last month
Citations as of Feb 12, 2019

Google ScholarTM



Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.