Citation: | Yuan Wei, Zhou Sheng, Lu Yajunet al. 3D numerical analysis for the effect between tip clearance and casing treatment in turbomachinery[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(09): 885-888. (in Chinese) |
[1] Koch C C. Experimental evaluation of outer case blowing or bleeding of single stage axial flow compressor . NASA CR-54592, 1970 [2]Hall E J, Crook A J, Delaney R A. Aerodynamic analysis of compressor casing treatment with a 3-D navier-stokes solver . AIAA Paper 94-2796,1994 [3] 李 玲. 轴流压气机机匣处理的数值模拟与实验研究 . 北京:北京航空航天大学动力系,1998 Li Ling. Numerical simulation and experimental research on casing treatment of axial flow compressor . Beijing:Dept of Jet Propulsion,Beijing University of Aeronautics and Astronautics,1998(in Chinese) [4] Wilke I, Kau H P. A numerical investigation of the influence of casing treatments on the tip leakage flow in a hpc front stage . ASME Paper, GT-2002-30642,2002
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