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Experimental study on combustion and flow resistance characteristics of an afterburner with air-cooled bluff-body flameholder

Chen, Yuqian LU ; Fan, Yuxin ; Bai, Xue Song LU ; Xu, Leilei LU ; Shan, Xu ; Bi, Yaning ; Deng, Yu and Han, Qixiang (2022) In Aerospace Science and Technology 123.
Abstract

In the afterburner assembled with an air-cooled bluff-body flameholder, cooling air is directly injected into the recirculation zone behind the bluff-body, which can reduce the local temperature and increase the oxygen concentration of the gas mixture in the wake of the bluff-body, thereby affecting the total pressure loss and combustion characteristics. To better understand the flow and combustion process of the system, the exhaust gas temperature, cold and hot total pressure losses in a rectangular premixed combustor are investigated under different cooling air jet conditions. Experimental results show that the added cooling air could improve the combustion efficiency and widen the blowout limit, whereas it could also give rise to an... (More)

In the afterburner assembled with an air-cooled bluff-body flameholder, cooling air is directly injected into the recirculation zone behind the bluff-body, which can reduce the local temperature and increase the oxygen concentration of the gas mixture in the wake of the bluff-body, thereby affecting the total pressure loss and combustion characteristics. To better understand the flow and combustion process of the system, the exhaust gas temperature, cold and hot total pressure losses in a rectangular premixed combustor are investigated under different cooling air jet conditions. Experimental results show that the added cooling air could improve the combustion efficiency and widen the blowout limit, whereas it could also give rise to an extra total pressure loss. However, when the cooling air flow rate was higher than a critical value, i.e., after the blowing ratio reached 2.5, the recirculation zone could be blown away, resulting in a failed ignition in the afterburner. Notably, the decreased temperature difference between the mainstream and the cooling air could improve the combustion efficiency and reduce the thermal resistance loss but enlarge the cold flow loss and hot total pressure loss. Moreover, since the oxygen content declined and autoignition appeared after the mainstream temperature reached 1100 K, the exhaust gas temperature and combustion efficiency declined rapidly, and the hot total pressure loss also decreased. In addition, with the fuel-gas ratio increasing, the combustion efficiency significantly dropped, the exhaust gas temperature and thermal resistance loss firstly increased to a peak value (at the equivalence ratio of 1.14) and then decreased for excessively fuel-rich combustion.

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author
; ; ; ; ; ; and
organization
publishing date
type
Contribution to journal
publication status
published
subject
keywords
Air-cooled flameholder, Cold flow loss, Combustion efficiency, Exhaust gas temperature, Thermal resistance loss, Total pressure loss
in
Aerospace Science and Technology
volume
123
article number
107488
publisher
Elsevier Masson SAS
external identifiers
  • scopus:85126950080
ISSN
1270-9638
DOI
10.1016/j.ast.2022.107488
language
English
LU publication?
yes
id
962a890f-4879-4354-ae06-af95ef5a6d40
date added to LUP
2022-04-19 12:59:40
date last changed
2022-04-19 17:00:43
@article{962a890f-4879-4354-ae06-af95ef5a6d40,
  abstract     = {{<p>In the afterburner assembled with an air-cooled bluff-body flameholder, cooling air is directly injected into the recirculation zone behind the bluff-body, which can reduce the local temperature and increase the oxygen concentration of the gas mixture in the wake of the bluff-body, thereby affecting the total pressure loss and combustion characteristics. To better understand the flow and combustion process of the system, the exhaust gas temperature, cold and hot total pressure losses in a rectangular premixed combustor are investigated under different cooling air jet conditions. Experimental results show that the added cooling air could improve the combustion efficiency and widen the blowout limit, whereas it could also give rise to an extra total pressure loss. However, when the cooling air flow rate was higher than a critical value, i.e., after the blowing ratio reached 2.5, the recirculation zone could be blown away, resulting in a failed ignition in the afterburner. Notably, the decreased temperature difference between the mainstream and the cooling air could improve the combustion efficiency and reduce the thermal resistance loss but enlarge the cold flow loss and hot total pressure loss. Moreover, since the oxygen content declined and autoignition appeared after the mainstream temperature reached 1100 K, the exhaust gas temperature and combustion efficiency declined rapidly, and the hot total pressure loss also decreased. In addition, with the fuel-gas ratio increasing, the combustion efficiency significantly dropped, the exhaust gas temperature and thermal resistance loss firstly increased to a peak value (at the equivalence ratio of 1.14) and then decreased for excessively fuel-rich combustion.</p>}},
  author       = {{Chen, Yuqian and Fan, Yuxin and Bai, Xue Song and Xu, Leilei and Shan, Xu and Bi, Yaning and Deng, Yu and Han, Qixiang}},
  issn         = {{1270-9638}},
  keywords     = {{Air-cooled flameholder; Cold flow loss; Combustion efficiency; Exhaust gas temperature; Thermal resistance loss; Total pressure loss}},
  language     = {{eng}},
  publisher    = {{Elsevier Masson SAS}},
  series       = {{Aerospace Science and Technology}},
  title        = {{Experimental study on combustion and flow resistance characteristics of an afterburner with air-cooled bluff-body flameholder}},
  url          = {{http://dx.doi.org/10.1016/j.ast.2022.107488}},
  doi          = {{10.1016/j.ast.2022.107488}},
  volume       = {{123}},
  year         = {{2022}},
}