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[1]尹 婷,吴高杨,聂万胜.压力振荡环境下液滴蒸发动态响应特性研究[J].火箭推进,2015,41(04):19-28.
 YIN Ting,WU Gaoyang,NIE Wansheng.Study on dynamic response characteristics of droplet evaporation in pressure oscillation environment[J].Journal of Rocket Propulsion,2015,41(04):19-28.
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压力振荡环境下液滴蒸发动态响应特性研究

参考文献/References:

[1]程心. 液体火箭发动机燃烧不稳定性[M]. 北京: 国防工业出版社, 1965.
[2]苏凌宇, 聂万胜, 刘卫东. 低频压力振荡环境下运动液滴蒸发过程的准稳态模型[J]. 推进技术, 2011, 32(5): 670- 675.
[3]YANG V. Liquid propellant rocket engine combustion in- stability[M]. USA: American Institute of Aeronautics & Astronautics, 1995.
[4]STRAHLE W C. A theoretical study of unsteady droplet burning: transients and periodic solutions[D]. Princeton, NJ: Department of Aeronautical Engineering, Princeton University, 1963.

[5]SHEU W J, LIOU N C. Effect of temporal variation of pressure on vaporization of liquid droplets[J]. International Journal of Heat and Mass Transfer. 1999(42): 4043-4054.

[6]YANG Vigor, MICHAEL M M. Liquid rocket motor combustion stability using coaxial injectors and super- critical droplet combustion and dynamics, SA-SA G- F49620-93-1-0126[R]. [S.l.]: [s.n.], 1995.
[7]OKAI K, MORIUE O, ARAKI M, et al. Combustion of single droplets and droplet pairs in a vibrating field under microgravity[J]. Proceeding of the Combustion Institute, 2000, 28: 977-983.
[8]TANABLE M, MORITA T, AOKI K, et al. Influence of standing sound waves on droplet combustion[J]. Procee- ding of the Combustion Institute, 2000, 28: 1007- 1013.
[9]TANABLE M, KUWAHARA T, SATOH K, et al. Droplet combustion in standing sound waves[J]. Proceeding of the Combustion Institute, 2005 (30): 1957-1964.

相似文献/References:

[1]汪广旭,刘占一,谭永华,等.燃烧室纵向压力振荡对燃料掺混过程的影响[J].火箭推进,2020,46(06):60.
 WANG Guangxu,LIU Zhanyi,TAN Yonghua,et al.Research on effects of longitudinal pressure oscillation on fuel mixing process in combustion chamber[J].Journal of Rocket Propulsion,2020,46(04):60.

备注/Memo

收稿日期:2015-01-12;修回日期:2015-03-20 基金项目:国家自然科学青年基金(51206185) 作者简介:尹婷(1990—),女,硕士研究生,研究领域为液体火箭发动机

更新日期/Last Update: 1900-01-01