[1] 刘存喜,刘富强,毛艳辉,等. 某型航空发动机用离心喷嘴燃油空间分布特性试验[J]. 航空动力学报,2013,28(4):783-791.LIU Cunxi,LIU Fuqiang,MAO Yanhui,et al. Experiment of fuel distribution of pressure-swirl atomizers for aero-engine[J]. Journal of Aerospace Power,2013,28(4):783-791. [2] LEFEBVRE A H. Fifty years of gas turbine fuel injection[J]. Atomization and Sprays,2000,10(3-5):251-276. [3] DONJAT D,ESTIVALEZES J L,MICHAU M,et al. Phenomenological study of the pressure swirl atomizer internal flow[C]//Proceedings of the 9th International Conference on Liquid Atomization and Spray Systems,Sorrento,Italy. 2003:12-19. [4] XIE Jinlong,GAN Rui,DUAN F,et al. Characterization of spray atomization and heat transfer of pressure swirl nozzles[J]. International Journal of Thermal Sciences,2013,68:94-102. [5] MA Hu,WU Xiaosong,FENG Feng,et al. An experimental study on fuel spray-induced vortex-like structures[J]. Experimental Thermal and Fluid Science,2014,57:335-343. [6] LI Tie,NISHIDA K,HIROYASU H. Droplet size distribution and evaporation characteristics of fuel spray by a swirl type atomizer[J]. Fuel,2011,90(7):2367-2376. [7] 岳明,杨茂林. 锥形液膜空间稳定性分析[J]. 航空动力学报,2003,18(6):794-798.YUE Ming,YANG Maolin. On the Spatial Instability of a conical Sheet[J]. Journal of Aerospace Power,2003,18(6):794-798. [8] 李继保,岳明,杨茂林. 锥形液膜Kevin-Helmholtz波不稳定性的实验研究[J]. 航天动力学报,2007,22(3):337-341.LI Jibao,YUE Ming,YANG Maolin. Experimental research of instability of kevin-helmholtz wave on conical sheets[J]. Journal of Aerospace Power,2007,22(3):337-341. [9] FU Qingfei,YANG Lijun,QU Yuanyuan,et al. Linear stability analysis of a conical liquid sheet[J]. Journal of Propulsion and Power,2010,26(5):955-968. [10] KIM D,IM J H,KOH H,et al. Effect of ambient gas density on spray characteristics of swirling liquid sheets[J]. Journal of Propulsion and Power,2007,23(3):603-611. [11] HOSSEINALIPOUR S M,GHORBANI R,KARIMEI H. Effect of liquid sheet and gas streams characteristics on the instability of a hollow cone spray using an improved linear instability analysis[J]. Asia-Pacific Journal of Chemical Engineering,2016,11(1):24-33. [12] KANG Zhongtao,WANG Zhenguo,LI Qinglian,et al. Effects of trumpet on the flow characteristics of pressure swirl injectors[J]. Journal of Propulsion and Power,2018,34(4):947-959. [13] RIZK N K,LEFEBVRE A H. Internal flow characteristics of simplex swirl atomizers[J]. Journal of Propulsion and Power,1985,1(3):193-199. [14] KIM S,KHIL T,KIM D,et al. Effect of geometric parameters on the liquid film thickness and air core formation in a swirl injector[J]. Measurement Science and Technology,2008,20(1):015403. [15] LIU Cunxi,LIU Fuqiang,YANG Jinhu,et al. Experimental investigation of spray and combustion performances of a fuel-staged low emission combustor:Effects of main swirl angle[J]. Journal of Engineering for Gas Turbines and Power,2017,139(12):121502. [16] LIU Cunxi,LIU Fuqiang,YANG Jinhu,et al. Experimental investigations of spray generated by a pressure swirl atomizer[J]. Journal of the Energy Institute,2019,92(2):210-221. [17] LIU Juan,ZHANG Xinqiao,LI Qinglian,et al. Effect of geometric parameters on the spray cone angle in the pressure swirl injector[J]. Proceedings of the Institution of Mechanical Engineers,Part G:Journal of Aerospace Engineering,2013,227(2):342-353. [18] KIM D,HAN P,YOON Y. Effect of flow condition and geometry on flow characteristics of a swirl injector[C/CD]//ILASS americas,16th Annual Conference on Liquid Atomization and Spray Systems,Monterey,CA. 2003. [19] 张新桥,沈赤兵,李清廉,等. 切向孔单/双排布局对离心式喷嘴锥形液膜雾化特性影响[J]. 推进技术,2016,37(11):2142-2149.ZHANG Xinqiao,SHEN Chibing,LI Qinglian,et al. Effects of single-row/dual-row layout of tangential holes on atomization characteristics of conical sheets emanating from swirl atomizer[J]. Journal of Propulsion Technology,2016,37(11):2142-2149. [20] 康忠涛,李清廉,张新桥,等. 气液同轴双离心式喷嘴喷雾特性[J]. 国防科技大学学报,2014(5):50-57.KANG Zhongtao,LI Qinglian,ZHANG Xinqiao,et al. Spary chatacteristic of gas-liquid double swirl coaxial injectr[J]. Journal of National University of Defense Technology,2014(5):50-57. |