| Citation: | ZHOU Tao, LI Feng, ZHAO Kai, et al. Effect of swirl numbers on flow characteristics of a concentric staged lean direct injection combustor[J]. Journal of Aerospace Power, 2022, 37(11):2488-2500 doi: 10.13224/j.cnki.jasp.20220290 |
A numerical investigation was conducted to study the effect of swirl numbers of the main stage and the pilot stage on the flow characteristics of a concentric staged lean direct injection (LDI) combustor. The swirl numbers at different reference cross-sections were used to measure the swirling intensity of the two stages respectively. The results showed that the width and reverse flow rate of the central recirculation zone (CRZ) increased with the increment of
| [1] |
LEFEBVRE A H,BALLAL D R. Gas turbine combustion:alternative fuels and emissions[M]. Boca Raton,US:CRC press,2010.
|
| [2] |
LILLEY D G. Swirl flows in combustion:a review[J]. AIAA Journal,1977,15(8): 1063-1078. doi: 10.2514/3.60756
|
| [3] |
LI G,ANGIER S,LAMBOLEZ O,et al. Experimental study of velocity flow field for a multiple swirl spray combustor[R]. Reno,US:40th AIAA Aerospace Sciences Meeting and Exhibit,2002.
|
| [4] |
AL-ABDELI Y M,MASRI A R. Stability characteristics and flowfields of turbulent non-premixed swirling flames[J]. Combustion Theory and Modelling,2003,7(4): 731-766. doi: 10.1088/1364-7830/7/4/007
|
| [5] |
HUANG Ying,YANG V. Effect of swirl on combustion dynamics in a lean-premixed swirl-stabilized combustor[J]. Proceedings of the Combustion Institute,2005,30(2): 1775-1782. doi: 10.1016/j.proci.2004.08.237
|
| [6] |
BA LAKRISHNAN P,SRINIVASAN K. Influence of swirl number on jet noise reduction using flat vane swirlers[J]. Aerospace Science and Technology,2018,73: 256-268. doi: 10.1016/j.ast.2017.11.039
|
| [7] |
FU Yongqiang,JENG S M,TACINA R. Characteristics of the swirling flow generated by an axial swirler[R]. ASME GT-2005-68728,2005.
|
| [8] |
吴垚锃,黄勇,王方,等. 不同结构多点喷射燃烧室冷态流场研究[J]. 航空动力学报,2010,25(7): 1536-1544. doi: 10.13224/j.cnki.jasp.2010.07.017
WU Yaozeng,HUANG Yong,WANG Fang,et al. Investigation of cold flow field of a multi-injection combustor with different geometries[J]. Journal of Aerospace Power,2010,25(7): 1536-1544. (in Chinese) doi: 10.13224/j.cnki.jasp.2010.07.017
|
| [9] |
FAROKHI S,TAGHAVI R,RICE E J. Effect of initial swirl distribution on the evolution of a turbulentjet[J]. AIAA Journal,1989,27(6): 700-706. doi: 10.2514/3.10168
|
| [10] |
LIANG Hanzhuang,MAXWORTHY T. An experimental investigation of swirling jets[J]. Journal of Fluid Mechanics,2005,525: 115-159. doi: 10.1017/S0022112004002629
|
| [11] |
TOH I K,HONNERY D,SORIA J. Axial plus tangential entry swirling jet[J]. Experiments in Fluids,2010,48(2): 309-325. doi: 10.1007/s00348-009-0734-2
|
| [12] |
İLBAŞ M,KARYEYEN S,YILMAZ İ. Effect of swirl number on combustion characteristics of hydrogen-containing fuels in a combustor[J]. International Journal of Hydrogen Energy,2016,41(17): 7185-7191. doi: 10.1016/j.ijhydene.2015.12.107
|
| [13] |
NICKOLAUS D A,CROCKER D S,BLACK D L,et al. Development of a lean direct fuel injector for low emission aero gas turbines[R]. ASME GT-2002-30409, 2002.
|
| [14] |
MONGIA H,AL-ROUB M,DANIS A,et al. Swirl cup modeling: Ⅰ[R]. Salt Lake City,US:37th Joint Propulsion Conference and Exhibit,2001.
|
| [15] |
LIU Yize,SUN Xiaoxiao,SETHI V,et al. Review of modern low emissions combustion technologies for aero gas turbine engines[J]. Progress in Aerospace Sciences,2017,94: 12-45. doi: 10.1016/j.paerosci.2017.08.001
|
| [16] |
闫东博,张群,汪玉明,等. 双级轴向旋流器性能评估方法:(一)综合旋流强度的影响[J]. 航空动力学报,2017,32(7): 1592-1598.
YAN Dongbo,ZHANG Qun,WANG Yuming,et al. Performance evaluation methods of two-stage axial swirler:Ⅰ influence of total swirling intensity[J]. Journal of Aerospace Power,2017,32(7): 1592-1598. (in Chinese)
|
| [17] |
赵自强,何小民,丁国玉,等. 旋流数组合对三级旋流流场的影响[J]. 推进技术,2016,37(10): 1909-1915. doi: 10.13675/j.cnki.tjjs.2016.10.014
ZHAO Ziqiang,HE Xiaoming,DING Guoyu,et al. Effects of swirl number combinations on flow characteristics of triple-swirlers[J]. Journal of Propulsion Technology,2016,37(10): 1909-1915. (in Chinese) doi: 10.13675/j.cnki.tjjs.2016.10.014
|
| [18] |
赵自强,何小民,丁国玉,等. 外旋流器旋流数对三级旋流流场特性的影响[J]. 航空动力学报,2017,32(2): 306-313. doi: 10.13224/j.cnki.jasp.2017.02.007
ZHAO Ziqiang,HE Xiaoming,DING Guoyu,et al. Effects of outer swirl number on flow characteristics of triple-swirlers[J]. Journal of Aerospace Power,2017,32(2): 306-313. (in Chinese) doi: 10.13224/j.cnki.jasp.2017.02.007
|
| [19] |
常峰,林宏军,程明,等. 低旋流中心分级燃烧室流场特性研究[J]. 推进技术,2020,41(6): 1334-1339. doi: 10.13675/j.cnki.tjjs.190430
CHANG Feng,LIN Hongjun,CHENG Ming,et al. Study on flow field characteristics of low swirl concentric staged combustor[J]. Journal of Propulsion Technology,2020,41(6): 1334-1339. (in Chinese) doi: 10.13675/j.cnki.tjjs.190430
|
| [20] |
VAN MAELE K,MERCI B,DICK E. Comparative study of k-epsilon turbulence models in inert and reacting swirling flows[R]. Orlando,US:33rd AIAA Fluid Dynamics Conference and Exhibit,2003
|
| [21] |
LAUNDER B E,SPALDING D B. The numerical computation of turbulent flows[J]. Computer Methods in Applied Mechanics and Engineering,1974,3(2): 269-289. doi: 10.1016/0045-7825(74)90029-2
|
| [22] |
CAI Jun,JENG S M,TACINA R. The structure of a swirl-stabilized reacting spray issued from an axial swirler[R]. Reno,US:43rd AIAA Aerospace Sciences Meeting and Exhibit,2005.
|
| [23] |
PATEL N,MENON S. Simulation of spray-turbulence-flame interactions in a lean direct injection combustor[J]. Combustion and Flame,2008,153(1/2): 228-257. doi: 10.1016/j.combustflame.2007.09.011
|
| [24] |
DEWANJI D,RAO A G. Spray combustion modeling in lean direct injection combustors:part I single-element LDI[J]. Combustion Science and Technology,2015,187(4): 537-557. doi: 10.1080/00102202.2014.965810
|