| [1] |
纪国剑.航空发动机典型篦齿封严泄漏特性的数值和实验研究[D].南京:南京航空航天大学,2008. JI Guojian.Numerical and experimental investigation of sealing characteristics on typical labyrinth seals in aeroengine[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2008.(in Chinese)
|
| [2] |
Soemarwoto B I,Kok J C,de Cock K M J.Performance evaluation of gas turbine labyrinth seals using computational fluid dynamics[R].ASME Paper 2007-GT-27905,2007.
|
| [3] |
Sturgess G J.Application of CFD to gas turbine engine secondary flow system:the labyrinth seal[R].AIAA 88-3203,1988.
|
| [4] |
Steinetz B M,Hendricks R C.Advanced seal technology role in meeting next generation turbine engine goals[R].NASA/TM-98-206961,1998.
|
| [5] |
David C J,Paul C I,John R T.Abradable stator gas turbine labyrinth seals:Part 2 numerical modeling of differing seal geometries and the construction of a second generation design tool[R].AIAA-2002-3937,2002.
|
| [6] |
李志刚,李军,丰镇平.蜂窝密封流动特性的数值研究和泄漏量计算公式的构造[J].机械工程学报,2011,47(2):142-148. LI Zhigang,LI Jun,FENG Zhenping.Numerical investigation on discharge behavior and predication formula establishment of leakage flow rate of honeycomb seal[J].Journal of Mechanical Engineering,2011,47(2):142-148.(in Chinese)
|
| [7] |
Chougule H H,Ramerth D.Numerical investigation of worn labyrinth seals[R].ASME Paper 06-GT-90690,2006.
|
| [8] |
张霞,张效伟,朱惠人,等.直通型篦齿封严特性的试验[J].航空动力学报,2010,25(8):1753-1757. ZHANG Xia,ZHANG Xiaowei,ZHU Huiren,et al.Experimental investigation on seal characteristics of straight-through labyrinth[J].Journal of Aerospace Power,2010,25(8):1753-1757.(in Chinese)
|
| [9] |
杨军.直通型封严篦齿流动特性的试验研究及数值计算[D].成都:电子科技大学,2009. YANG Jun.Experimental investigation and numerical study of straight-through labyrinth characteristic of flow[D].Chengdu:University of Electronic Science and Technology of China,2009.(in Chinese)
|
| [10] |
Willenborg K,Kim S,Wittig S.Effects of Reynolds number and pressure ratio on leakage loss and heat transfer in a stepped labyrinth seal[R].ASME Paper 2001-GT-0123,2001.
|
| [11] |
Gamal A M,Vance J M.Labyrinth seal leakage tests:tooth profile,tooth thickness,and eccentricity effects[R].ASME Paper 2007-GT-27223,2007.
|
| [12] |
黄晓光,吴丁毅,王泳泓,等.航空发动机中直通式篦齿密封腔内流动和换热的实验研究[J].航空动力学报,2000,15(2):159-162. HUANG Xiaoguang,WU Dingyi,WANG Yonghong,et al.Experimental investigation of flow and heat transfer in straight labyrinth seal[J].Journal of Aerospace Power,2000,15(2):159-162.(in Chinese)
|
| [13] |
王鹏飞,刘玉芳,郭文,等.高转速对直通型篦齿封严特性影响的试验研究[J].燃气涡轮试验与研究,2007,20(2):45-48. WANG Pengfei,LIU Yufang,GUO Wen,et al.Influence of high rotational speeds on the labyrinth sealing characteristics[J].Gas Turbine Experiment and Research,2007,20(2):45-48.(in Chinese)
|
| [14] |
Denecke J,Dullenkopf K,Wittig S.Experimental investigation of the total temperature increase and swirl development in rotating labyrinth seals[R].ASME Paper 2005-GT-68677,2005.
|
| [15] |
王鹏飞,郭文,张靖周.旋转封严篦齿风阻温升的试验研究与数值分析[J].航空动力学报,2013,28(6):1402-1408. WANG Pengfei,GUO Wen,ZHANG Jingzhou.Experiment investigation and numerical analysis of windage heating in rotating labyrinth seal[J].Journal of Aerospace Power,2013,28(6):1402-1408.(in Chinese)
|
| [16] |
Braun E,Dullenkopf K,Bauer H J.Optimization of labyrinth seal performance combining experimental,numerical and data mining methods[R].ASME Paper 2012-GT-68077,2012.
|
| [17] |
夏全忠.直通型封严篦齿瞬稳态特性研究[D].西安:西北工业大学,2012. XIA Quanzhong.Investigations transient-static properties of straight-through labyrinth seal[D].Xi'an:Northwestern Polytechnical University,2012.(in Chinese)
|
| [18] |
Childs P R N.Rotating flow[M].Burlington,US:Butterworth-Heinemann,2011.
|
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