| Citation: | KANG Yudong, ZHONG Shilin, PENG Weikang, et al. Flow and combustion characteristics of trapped vortex cavity combined with radial flameholder[J]. Journal of Aerospace Power, 2025, 40(1):20230128 doi: 10.13224/j.cnki.jasp.20230128 |
In order to improve the comprehensive combustion performance of trapped vortex cavity afterburner and better understand the effect of radial flameholder installation angle on flow and combustion characteristics, numerical and experimental investigation were employed at 5°, 8°, 10°, 15° under different excess air coefficients. The investigations were performed under the bypass temperature 600 K, the core temperature
| [1] |
HSU K,GROSS L,TRUMP D,et al. Performance of a trapped-vortex combustor[R]. AIAA-95-0810,1995.
|
| [2] |
HSU K Y,GOSS L P,ROQUEMORE W M. Characteristics of a trapped-vortex combustor[J]. Journal of Propulsion and Power,1998,14(1): 57-65. doi: 10.2514/2.5266
|
| [3] |
STURGESS G,HSU K. Entrainment of mainstream flow in a trapped-vortex combustor[R]. AIAA-97-0261,1997.
|
| [4] |
郭煜玺,何小民,朱一骁,等. 单凹腔驻涡燃烧室值班油气匹配研究[J]. 推进技术,2021,42(3): 578-586. GUO Yuxi,HE Xiaomin,ZHU Yixiao,et al. Matching of fuel and air in pilot stage of single-cavity trapped vortex combustor[J]. Journal of Propulsion Technology,2021,42(3): 578-586. (in Chinese
GUO Yuxi, HE Xiaomin, ZHU Yixiao, et al. Matching of fuel and air in pilot stage of single-cavity trapped vortex combustor[J]. Journal of Propulsion Technology, 2021, 42(3): 578-586. (in Chinese)
|
| [5] |
DAVOUDZADEH F,BUEHRLE R,LIU N S,et al. Numerical simulation of the RTA combustion rig[R]. NASA/TM 2005-213899,2005.
|
| [6] |
MCNELIS N B,BARTOLOTTA P. Revolutionary turbine accelerator (RTA) demonstrator[R]. AIAA 2005-3250,2005.
|
| [7] |
LEE J,WINSLOW R,BUEHRLE R J. The GE-NASA RTA hyperburner design and development[R]. NASA/TM 2005-213803,2005.
|
| [8] |
KOSHOFFER J M. Trapped vortex cavity afterburner: US7225623[P]. 2007-06-05.
|
| [9] |
VERMEERSCH M L. Externally fueled trapped vortex cavity augmentor: US7467518[P]. 2008-12-23.
|
| [10] |
WOLTMANN I E,ARCHER S S,BACHMAN F G,et al. Augmentor with trapped vortex cavity pilot: US8011188[P]. 2011-09-06.
|
| [11] |
BACHMAN F G,LEWIS R L,BOCKWICH R S,et al. Ejector purge of cavity adjacent exhaust flowpath: US 8726670[P]. 2014-05-20.
|
| [12] |
秦伟林,何小民,金义,等. 凹腔驻涡与支板稳焰组合加力燃烧室模型冷态流场试验[J]. 航空动力学报,2012,27(6): 1347-1354. QIN Weilin,HE Xiaomin,JIN Yi,et al. Experimental investigation on cold flow characteristics of afterburner with cavity/strut hybrid flameholders[J]. Journal of Aerospace Power,2012,27(6): 1347-1354. (in Chinese
QIN Weilin, HE Xiaomin, JIN Yi, et al. Experimental investigation on cold flow characteristics of afterburner with cavity/strut hybrid flameholders[J]. Journal of Aerospace Power, 2012, 27(6): 1347-1354. (in Chinese)
|
| [13] |
ZHU Zhixin,HE Xiaomin,XUE Chong,et al. Experimental investigations on combustion characteristics of a cavity pilot augmentor of the turbine-based combined cycle engine[J]. Proceedings of the Institution of Mechanical Engineers: Part G Journal of Aerospace Engineering,2015,229(11): 2024-2034. doi: 10.1177/0954410014564202
|
| [14] |
ZHU Zhixin,HUANG Yakun,ZHANG Huangwei,et al. Combustion performance in a cavity-based combustor under subatmospheric pressure[J]. Fuel,2021,302: 121115. doi: 10.1016/j.fuel.2021.121115
|
| [15] |
谭云川,钟华贵,孙瑞礼,等. 驻涡加力燃烧室贫油熄火性能的影响[J]. 航空动力学报,2021,36(9): 1932-1941. TAN Yunchuan,ZHONG Huagui,SUN Ruili,et al. Effect of lean blowout performance of trapped vortex combustor of the afterburner[J]. Journal of Aerospace Power,2021,36(9): 1932-1941. (in Chinese
TAN Yunchuan, ZHONG Huagui, SUN Ruili, et al. Effect of lean blowout performance of trapped vortex combustor of the afterburner[J]. Journal of Aerospace Power, 2021, 36(9): 1932-1941. (in Chinese)
|
| [16] |
于文博,范育新,岳晨,等. 一种蒸发式凹腔驻涡值班稳定器的流动与点火性能研究[J]. 推进技术,2023,44(5): 108-117. YU Wenbo,FAN Yuxin,YUE Chen,et al. Flow characteristics and ignition performance analysis of an evaporating cavity trapped vortex pilot flame-holder[J]. Journal of Propulsion Technology,2023,44(5): 108-117. (in Chinese
YU Wenbo, FAN Yuxin, YUE Chen, et al. Flow characteristics and ignition performance analysis of an evaporating cavity trapped vortex pilot flame-holder[J]. Journal of Propulsion Technology, 2023, 44(5): 108-117. (in Chinese)
|
| [17] |
JIN Yi,HE Xiaomin,JIANG Bo,et al. Effect of cavity-injector/radial-strut relative position on performance of a trapped vortex combustor[J]. Aerospace Science and Technology,2014,32(1): 10-18. doi: 10.1016/j.ast.2013.12.014
|
| [18] |
吴伟秋,范育新,缪俊杰,等. 壁式与径向组合稳定器的流动与点火特性研究[J]. 推进技术,2022,43(7): 308-315. WU Weiqiu,FAN Yuxin,MIAO Junjie,et al. Flow and ignition characteristics of wall combined with radial flame-holder[J]. Journal of Propulsion Technology,2022,43(7): 308-315. (in Chinese
WU Weiqiu, FAN Yuxin, MIAO Junjie, et al. Flow and ignition characteristics of wall combined with radial flame-holder[J]. Journal of Propulsion Technology, 2022, 43(7): 308-315. (in Chinese)
|