Investigation of Pressure Rise and Flame Acceleration Characteristics in a Single Channel of Wave Rotor Combustor with Spoilers

A simplified single channel wave rotor combustor (WRC) experimental rig was established, in which the spoilers with different blockage ratios (BR) could be conveniently installed and disassembled. The spoilers were firstly used for WRC to improve the pressure rise. The effects of different blockage...

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Main Authors: Jianzhong Li, Kaichen Zhang, Wei Li, Li Yuan
Format: Article
Language:English
Published: Hindawi Limited 2019-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2019/6259204
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spelling doaj-41c9c423f7834cbcb4ee679bb710ced22020-11-25T01:35:52ZengHindawi LimitedInternational Journal of Aerospace Engineering1687-59661687-59742019-01-01201910.1155/2019/62592046259204Investigation of Pressure Rise and Flame Acceleration Characteristics in a Single Channel of Wave Rotor Combustor with SpoilersJianzhong Li0Kaichen Zhang1Wei Li2Li Yuan3Key Laboratory of Aero-Engine Thermal Environment and Structure, Ministry of Industry and Information Technology, Nanjing University of Aeronautics and Astronautics, 29 Yudao St., Nanjing 210016, ChinaKey Laboratory of Aero-Engine Thermal Environment and Structure, Ministry of Industry and Information Technology, Nanjing University of Aeronautics and Astronautics, 29 Yudao St., Nanjing 210016, ChinaAVIC Aviation Powerplant Research Institute, 1815 Rd., Zhuzhou 412002, ChinaSchool of National Defense Engineering, The Army Engineering University of PLA, 88 Biaoying Rd., Nanjing 210007, ChinaA simplified single channel wave rotor combustor (WRC) experimental rig was established, in which the spoilers with different blockage ratios (BR) could be conveniently installed and disassembled. The spoilers were firstly used for WRC to improve the pressure rise. The effects of different blockage ratios on the pressure rise and flame acceleration characteristics in a single channel of the WRC were investigated. The addition of spoilers could remarkably improve the pressure rise and flame propagation speed in a single channel of the WRC. While the blockage ratio of the spoiler increases, both pressure rise and mean flame propagation speed are improved. When the spoilers with a blockage ratio of 38.91% are used, the peak pressure increases by 200% compared to that of WRC without the spoilers. When the spoilers of different blockage ratios (23.35%, 31.13%, and 38.91%) are used, it is found that the flame propagation speed is significantly improved with the increasing of the blockage ratio. Specifically, the maximum flame propagation speed reaches 55 m/s, and the maximum mean flame propagation speed is 36.95 m/s. Furthermore, combustion becomes more intense, and the flame is brighter around the spoiler.http://dx.doi.org/10.1155/2019/6259204
collection DOAJ
language English
format Article
sources DOAJ
author Jianzhong Li
Kaichen Zhang
Wei Li
Li Yuan
spellingShingle Jianzhong Li
Kaichen Zhang
Wei Li
Li Yuan
Investigation of Pressure Rise and Flame Acceleration Characteristics in a Single Channel of Wave Rotor Combustor with Spoilers
International Journal of Aerospace Engineering
author_facet Jianzhong Li
Kaichen Zhang
Wei Li
Li Yuan
author_sort Jianzhong Li
title Investigation of Pressure Rise and Flame Acceleration Characteristics in a Single Channel of Wave Rotor Combustor with Spoilers
title_short Investigation of Pressure Rise and Flame Acceleration Characteristics in a Single Channel of Wave Rotor Combustor with Spoilers
title_full Investigation of Pressure Rise and Flame Acceleration Characteristics in a Single Channel of Wave Rotor Combustor with Spoilers
title_fullStr Investigation of Pressure Rise and Flame Acceleration Characteristics in a Single Channel of Wave Rotor Combustor with Spoilers
title_full_unstemmed Investigation of Pressure Rise and Flame Acceleration Characteristics in a Single Channel of Wave Rotor Combustor with Spoilers
title_sort investigation of pressure rise and flame acceleration characteristics in a single channel of wave rotor combustor with spoilers
publisher Hindawi Limited
series International Journal of Aerospace Engineering
issn 1687-5966
1687-5974
publishDate 2019-01-01
description A simplified single channel wave rotor combustor (WRC) experimental rig was established, in which the spoilers with different blockage ratios (BR) could be conveniently installed and disassembled. The spoilers were firstly used for WRC to improve the pressure rise. The effects of different blockage ratios on the pressure rise and flame acceleration characteristics in a single channel of the WRC were investigated. The addition of spoilers could remarkably improve the pressure rise and flame propagation speed in a single channel of the WRC. While the blockage ratio of the spoiler increases, both pressure rise and mean flame propagation speed are improved. When the spoilers with a blockage ratio of 38.91% are used, the peak pressure increases by 200% compared to that of WRC without the spoilers. When the spoilers of different blockage ratios (23.35%, 31.13%, and 38.91%) are used, it is found that the flame propagation speed is significantly improved with the increasing of the blockage ratio. Specifically, the maximum flame propagation speed reaches 55 m/s, and the maximum mean flame propagation speed is 36.95 m/s. Furthermore, combustion becomes more intense, and the flame is brighter around the spoiler.
url http://dx.doi.org/10.1155/2019/6259204
work_keys_str_mv AT jianzhongli investigationofpressureriseandflameaccelerationcharacteristicsinasinglechannelofwaverotorcombustorwithspoilers
AT kaichenzhang investigationofpressureriseandflameaccelerationcharacteristicsinasinglechannelofwaverotorcombustorwithspoilers
AT weili investigationofpressureriseandflameaccelerationcharacteristicsinasinglechannelofwaverotorcombustorwithspoilers
AT liyuan investigationofpressureriseandflameaccelerationcharacteristicsinasinglechannelofwaverotorcombustorwithspoilers
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