[1] DENTON J D. Loss mechanism in turbomachines[J]. Journal of Turbomachinery, 1993, 115(4):621-656.
[2] BOHN D E, KREWINKEL R, TUMMERS C, et al. Influence of the radial and axial gap of the shroud cavities on the flow field in a 2-stage turbine[R]. ASME, 2006.
[3] ROSIC B, DENTON J D. Control of shroud leakage loss by reducing circumferential mixing[J]. ASME Journal of Turbomachinery, 2008, 130:1-7.
[4] ZIMMERMANN H. Air system correlations part(1):labyrinth seal[R]. ASME, 1998.
[5] NIRMALAN N V, BAILEY J C. Experimental investigation of aerodynamic losses of different shapes of a shrouded blade tip section[R]. ASME, 2005.
[6] 吴丁毅. 两类常用篦齿密封和临界特性的分析与比较[J]. 航空动力学报, 1997, 12(4):397-400.
WU D Y. Comparison between two kinds of conventional labyrinth[J]. Journal of Aerospace Power, 1997, 12(4):397-400.
[7] 鄢景, 杨自春. 动力涡轮有冠及无冠叶栅顶部二次流的数值分析[J]. 燃气轮机技术, 2011, 24(2):30-34.
YAN J, YANG Z C. Numerical analysis of tip secondary flow in rotor cascades with or without shroud in power turbine[J]. Gas Turbine Technology, 2011, 24(2):30-34.
[8] 李钰洁, 刘永葆, 高杰. 间隙流动对涡轮叶片温度场分布影响的数值研究[J]. 海军工程大学学报, 2013, 6(25):24-29.
LI Y J, LIU Y B, GAO J. Numerical analysis of effect of clearance flow on distribution of temperature field in turbine blade[J]. Journal of Naval University of Engineering, 2013, 6(25):24-29.
[9] 黄晓光,吴丁毅. 封严篦齿腔内流动及旋涡分布和顶板换热特性的实验研究[J]. 流体力学实验与测量, 2000, 14(4):20-25.
HUANG X G, WU D Y. The investigation of flow field and heat transfer in cavity of labyrinth seal[J]. Experiments and Measurements in Fluid Mechanics, 2000, 14(4):20-25.
[10] 刘高文, 蒋兆午, 务为涛, 等. 基于数值模拟的矩形凹槽对直通型篦齿封严特性影响研究[J]. 推进技术, 2013, 34(2):181-186.
LIU G W, JIANG Z W, WU W T, et al. Investigation on effects of rectangular groove on leakage of straight-trough labyrinth seal based on numerical simulation[J]. Journal of Propulsion Technology, 2013,34(2):181-186.
[11] 高杰, 郑群, 李义进. 动叶顶部蜂窝面迷宫密封对涡轮级气动性能的影响[J]. 航空动力学报, 2012, 27(1):160-168.
GAO J, ZHENG Q, LI Y J. Effect of labyrinth-honeycomb seal of shrouded rotor blades on the aerodynamic performance of the turbine stage[J]. Journal of Aerospace Power, 2012, 27(1):160-168.
[12] 贾惟, 刘火星. 涡轮叶栅叶冠泄漏流动数值研究[J]. 推进技术, 2013, 34(3):316-325.
JIA W, LIU H X. Numerical investigation on shroud leakage flow in turbine cascade[J]. Journal of Propulsion Technology, 2013, 34(3):316-325.
[13] 马石.刘永葆.缪四春, 等. 叶冠齿顶间隙对涡轮气动性能的影响研究[J]. 机械工程与自动化, 2015 (2):29-31.
MA S, LIU Y B, MIU S C, et al. Effect of tip clearance on aerodynamic performance of turbine[J]. Mechanical Engineering & Automation, 2015(2):29-31.