4.7 Article

Dependence of the blowout limit on flow structure, heat transfer, and pressure loss in a bluff-body micro-combustor

期刊

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY
卷 45, 期 38, 页码 19912-19925

出版社

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.ijhydene.2020.04.113

关键词

Micro-combustor; Bluff body; Blowout limit; Blockage ratio; Pressure loss

资金

  1. National Key Research and Development Program of China [2017YFC0212605]
  2. National Natural Science Foundation of China [51506069]
  3. Young Elite Scientists Sponsorship Program by CAST [2018QNRC001]
  4. Fundamental Research Funds for the Central Universities [HUST2016YXMS286]

向作者/读者索取更多资源

In this study, we numerically investigated the main factors affecting the flame blowout limit of bluff-body micro-combustors with a blockage ratio (delta) varying from 0.3 to 0.8; the combustion performance of these combustors is investigated as well. Measurements from the literature (Fan et al., 2012, Int J Hydrogen Energy, 37, 19,190-19,197) were used to validate the present numerical models. The predicted results are in good agreement with the experimental data, with a relative error of less than 10%. The results show that the blowout limit increases with delta in a non-monotonic manner. The establishment of a low-velocity recirculation behind the bluff body and recirculation of heat and key radicals help increase the flame blowout limit, whereas the stretching of reaction zones has an unfavorable effect. In contrast, heat loss contributes negligibly to the difference between the blowout limits in the micro-combustors for different values of S. An extra pressure loss or initial power input is required to improve the blowout limits. An available size of the in- built bluff body should be carefully selected to maximize its efficiency and to considerably improve the blowout limit; however, this should be realized while ensuring a low cost of pressure loss when designing a micro-combustor. In general, delta = 0.5 is relatively optimal and recommended for the straight combustion channel discussed herein. (C) 2020 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.

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