[1] 曹玉璋.航空发动机传热学[M].北京:北京航空航天大学出版社,2005.
[2] Zimmermann H.Air System Correlations Part (1):Labyrinth Seal[R].ASME 98-GT-208.
[3] 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,0,4(4):20-25.
[4] Roger P, David C.Advanced Seal Rig Experiments and Analysis[R].AIAA 2005-4150.
[5] 吴丁毅,刘振侠.交错式篦齿封严特性的实验研究[J].推进技术,1997,18(2).(WU Ding-yi,LIU Zhen-xia.An Experimental Investigation on Sealing Characteristics of Interlacing Labyrinth[J].Journal of Propulsion Technology,7,8(2).)
[6] 王鹏飞,郭文.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,7,0(2).
[7] 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,0,5(8):1753-1757.
[8] Tim P.Modelling the Labyrinth Seal Discharge Coefficient Using Data Mining Methods[R].ASME 2010-GT-22661.
[9] Erik B, Klaus D,Hans J B.Optimization of Combining Experimental, Numerical and Data Mining Methods[R].ASME 2012-GT-68077.
[10] Denecke J, Schramm V, Kim S, et al.Influence of Rub-Grooves on Labyrinth Seal Leakage[J]. ASME Journal of Turbomachinery, 3,5(4):387-393.
[11] Rhode D L,Adams R G.Rub-Groove Width and Depth Effects on Flow Predictions for Straight-Through Labyrinth Seals[J].Journal of Tribology, 4,6(3).
[12] 纪国剑,齿间环形凹槽结构对直通篦齿封严特性影响的数值研究[J].流体机械,7,5(12):21-24.
[13] 纪国剑, 吉洪湖.直通篦齿静止衬套上磨损槽对泄漏特性影响的数值研究[J].航空动力学报,8,3(8).
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