欢迎登录材料期刊网

材料期刊网

高级检索

燃气涡轮发动机中的冷气与主流掺混会带来一定的气动损失,造成发动机总体性能下降.本文在三维N-S程序的基础上,引入一种较为简单的冷气射流计算模型,对一级高压涡轮含有冷气掺混的三维流场进行了数值分析,揭示了冷气掺混对导叶流量特性及损失分布的影响,并通过涡轮叶片排二次流动结构的分析初步探讨了冷气掺混损失机理.

参考文献

[1] Bohn D.Prediction of the Film-Cooling Effective ness in Gas Turbine Blades Using a Numerical Model for the Coupled Simulation of Fluid Flow and Diabatic Walls[A].,1995:1150-1159.
[2] Bohn D et al.3-D Numerical Simulation of the Flow Through a Turbine Blade Cascade with Cooling Injection at the Leading Edge[Z].ASME 97-GT-247,1997.
[3] Haselhause A;Vogel D T .Nuimerical Simulation of Tur bine Blade Cooling with Respect to Blade Heat Conduction and Inlet Inlet Temperature Profiles[R].AIAA 95-3041,1995.
[4] Kao K H;Liu M S .On the Application of Chimera/Unstructed Hybrid Grids for Conjugate Heat Transfer[R].ASME 96-GT-165,1996.
[5] V Michelassi et al.Aerodynamic Performance of A Tran sonic Turbine Guide Vane with Trailing Edge Coolant Ejection Part II Numerical Approach[R].ASME Paper 94GT-248,1994.
[6] 陈浮,王仲奇,冯国泰.跨音速旋转气冷涡轮叶栅流场计算研究[C].中国工程热物理学会热机气动热力学学术会议论文集,1998:Ⅱ-43~Ⅱ-47.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%