Effects of nonaxisymmetric tip clearance on axial compressor performance and stability

被引：0
|
作者：
Graf, M.B. [1 ]
Wong, T.S. [1 ]
Greitzer, E.M. [1 ]
Marble, F.E. [1 ]
Tan, C.S. [1 ]
Shin, H.-W. [2 ]
Wisler, D.C. [2 ]
机构：
[1] Gas Turbine Laboratory, Massachusetts Inst. of Technology, Cambridge, MA 02139, United States
[2] Aero Technology Laboratories, GE Aircraft Engines, Cincinnati, OH 45215, United States
来源：
Journal of Turbomachinery | 1998年 / 120卷 / 04期
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页码：648 / 661
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