Mach Number Effects on Turbine Blade Transition Length Prediction
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[1] J. P. Clark,et al. On the propagation of naturally-occurring turbulent spots , 1994 .
[2] M. E. McCormick,et al. An Analysis of the Formation of Turbulent Patches in the Transition Boundary Layer , 1968 .
[3] R. E. Mayle,et al. The Role of Laminar-Turbulent Transition in Gas Turbine Engines , 1991 .
[4] H. Lomax,et al. Thin-layer approximation and algebraic model for separated turbulent flows , 1978 .
[5] M. Liou,et al. Navier-Stokes solution of transonic cascade flows using nonperiodic C-type grids , 1992 .
[6] Rodrick V. Chima,et al. Explicit multigrid algorithm for quasi-three-dimensional viscous flows in turbomachinery , 1987 .
[7] Tony Arts,et al. Aero-Thermal Performance Measurements and Analysis of a Two-Dimensional High Turning Rotor Blade , 1997 .
[8] M. S. Mihelc,et al. Analytical and Experimental Evaluation of the Heat Transfer Distribution over the Surfaces of Turbine Vanes , 1983 .
[9] N. A. Thyson,et al. Extension of Emmons' spot theory to flows on blunt bodies , 1971 .
[10] J. S. Milne,et al. End-Stage Boundary Layer Transition Models for Engineering Calculations , 1994 .
[11] Roddam Narasimha,et al. The laminar-turbulent transition zone in the boundary layer , 1985 .
[12] H. W. Emmons,et al. The Laminar-Turbulent Transition in a Boundary Layer-Part I , 1951 .