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[1]王晓锋,李昌奂,韩 飞,等.动叶顶部间隙结构对涡轮性能影响的数值分析[J].火箭推进,2013,39(02):24-28.
 WANG Xiao-feng LI Chang-huan HAN Fei CHEN Ben-sen.Numerical analysis on influence of rotor tip clearance structure on turbine performance[J].Journal of Rocket Propulsion,2013,39(02):24-28.
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动叶顶部间隙结构对涡轮性能影响的数值分析

参考文献/References:

[1]张国舟, 俞南嘉, 魏沫. 液体火箭发动机反力式涡轮动叶进口攻角的研究[J]. 推进技术, 2002, 23(5): 383-386.
[2]庄毓南, 张国舟, 刘中祥, 等. 液体火箭发动机高效率反力式涡轮的设计[J]. 北京航空航天大学学报, 1999, 25(6): 696-699.
[3]祖国君, 张远君. 影响液体火箭发动机涡轮效率的某些因素分析[J]. 推进技术, 1992 (6): 38-43.
[4]李斌, 王晓锋, 陈本森, 等. 大叶顶间隙高效率火箭发动机涡轮设计[J]. 宇航学报, 2009, 30(2): 695-698.
[5]ОВСЯННИКОВ Б В, БОРОВСКИЙ Б И. Теория и расчёт агрегатов питания жидкостных ракетных двигателей[M]. МОСКВА, МАШИНОСТРОЕНИЕ: [s.n.], 1986.
[6]HELMERS L, KLINGMANN J. Unshrouded rotor tip clearance effects in expander cycle turbines[C]// Proceedings of the ASME Turbo Expo. New York: American Society of Mechanical Engineers, 2002: 111-121.

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备注/Memo

收稿日期:2012-11-06;修回日期:2012-12-28
基金项目:中国航天科技集团公司支撑项目(2008JY07)
作者简介:王晓锋(1976—),男,高级工程师,研究领域为液体火箭发动机涡轮泵设计

更新日期/Last Update: 1900-01-01