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本文对某空冷汽轮机马刀叶片性能进行了不同工况三维数值分析.计算表明,所计算的低压缸马刀型在设计工况条件下,流动状况良好.在非设计工况,即小流量工况条件下,除第一级静叶以外,其余叶片排都存在大负攻角流动.

参考文献

[1] Mark G Turner;Paul H Vitt et al.Multistage Simulations of the GE90 Turbine[R].99-GT-98,1999.
[2] Y S Li;R G Wells .The Three-Dimensional Aerodynamic Design and Tests of a Three-Stage Transonic Compressor[R].99-GT-68,1999.
[3] Edward Hall .Aerodynamic Modeling of Multistage Compressor Flowfields-Part 1: Analysis of Rotor/Stator/Rotor Aerodynamic Interaction[R].97-GT-344,1997.
[4] Wolfgang Elmendorf;Frank Mildner et al.ThreeDimensional Analysis of a Multistage Compressor Flow Field[R].98-GT-249,1998.
[5] Nozaki K Kikuchi;T Nishizawa;Y Matsuo .Unsteady Three-Dimensional Viscous Flow Computations of Multiple-Blade-Row Interactions[R].ISABE 99-70,1999.
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