LEADING EDGE FILM-COOLING EFFECTS ON TURBINE BLADE HEAT TRANSFER

References

• R. J. Goldstein , Film Cooling, in T. F. Irvine , Jr . and J. P. Hartnett ( eds. ), Advances in Heat Transfer , vol. 7 ,pp. 321 – 379 , Academic , New York , 1971 .
   Google Scholar
• V. K. Garg and R. E. Gaugler , Heat Transfer in Film-Cooled Turbine Blades , ASME Paper 93-GT-81 , 1993 .
   Google Scholar
• V. K. Garg and R. E. Gaugler , Prediction of Film Cooling on Gas Turbine Airfoils , ASME Paper 94-GT-16 , 1994 .
   Google Scholar
• J. P. Bons , C. D. MacArthur , and R. B. Rivir , The Effect of High Freestream Turbulence on Film Cooling Effectiveness , ASME Paper 94-GT-51 , 1994 .
   Google Scholar
• J. S. Lee , S. T. Ro , and H. J. Seo , Mass Transfer Effects of Free-Stream Turbulence and Horseshoe Vortex Formed at the Upstream Edge of Film Cooling Jets About a Cylindrical Surface , ASME Paper 94-GT-18 , 1994 .
   Google Scholar
• M. Y. Jabbari , K. C. Marston , E. R. G. Eckert , and R. J. Goldstein , Film Cooling of the Gas Turbine Endwall by Discrete-Hole Injection , ASME Paper 94-GT-67 , 1994 .
   Google Scholar
• B. Sen , D. L. Schmidt , and D. G. Bogard , Film Cooling with Compound Angle Holes Heat Transfer , ASME Paper 94-GT-3H , 1994 .
   Google Scholar
• D. L. Schmidt , B. Sen , and D. G. Bogard , Film Cooling with Compound Angle Holes Adiabatic Effectiveness , ASME Paper 94-GT-312 , 1994 ,
   Google Scholar
• Y. W. Kim , W. Abdel-Messeh , J. P. Downs , F. O. Soechting , G. D. Steuber , and S. Tanrikut , A Summary of the Cooled Turbine Blade Tip Heat Transfer and Film Effectiveness Investigations Performed by Dr. D. E . Metzger, ASME Paper 94-GT-167 , 1994 .
   Google Scholar
• N. Hay , D. Lampard , and A. Khaldi , The Coefficient of Discharge of 30° Inclined Film Cooling Holes with Rounded Entries or Exits , ASME Paper 94-GT-180 , 1994 .
   Google Scholar
• J. M. Fougeres and R. Heider , Three-Dimensional Navier-Stokes Prediction of Heat Transfer with Film Cooling , ASME Paper 94-GT-14 , 1994 .
   Google Scholar
• B. Weigand and S. P. Harasgama , Computations of a Film Cooled Turbine Rotor Blade with Non-Uniform Inlet Temperature Distribution Using a Three-Dimensional Viscous Procedure , ASME Paper 94-GT-15 , 1994 .
   Google Scholar
• W. N. Dawes , The Extension of a Solution-Adaptive Three-Dimensional Navier-Stokes Solver Toward Geometries of Arbitrary Complexity , J. Turbomach. , vol. n115 n, pp. 283 – 295 , 1993 .
   Google Scholar
• E. J. Hall , D. A. Topp , and R. A. Delaney , Aerodynamic/Heat Transfer Analysis of Discrete Site Film-Cooled Turbine Airfoils , AIAA Paper 94 – 3070 , 1994 .
   Google Scholar
• R. J. Boyle and P. Giel , Three-Dimensional Navier-Stokes Heat Transfer Predictions for Turbine Blade Rows , AIAA Paper 92 – 3068 , 1992 .
   Google Scholar
• A. Arnone , M.-S. Liou , and L. A. Povinelli , Multigrid Calculation of Three-Dimensional Viscous Cascade Flows , AIAA Paper 91 – 3238 , 1991 .
   Google Scholar
• L. D. Hylton , V. Nirmalan , B. K. Sultanian , and R. M. Kaufman , The Effects of Leading Edge and Downstream Film Cooling on Turbine Vane Heat Transfer , NASA CR 182133 , 1988 .
   Google Scholar
• J. S. Liu , R. Utz , and R. Bozzola , Aerodynamic Design and Analysis of a Gas Producer Turbine Stator with Film Cooling Injection , AIAA Paper 94 – 2928 , 1994 .
   Google Scholar
• J. H. Leylek and R. D. Zerkle , Discrete-Jet Film Cooling A Comparison of Computational Results with Experiments , J. Turbomach. , vol, n116 n, pp. 358 – 368 , 1994 .
   Google Scholar
• H. Schlichting , Boundary Layer Theory , 7th ed. , p. 328 , McGraw-Hill , New York , 1979 .
   Google Scholar
• B. S. Baldwin and H. Lomax , Thin-Layer Approximation and Algebraic Model for Separated Turbulent Flows , AIAA Paper 78 – 257 , 1978 .
   Google Scholar
• A. A. Ameri and A. Arnone , Transition Modeling Effects on Turbine Rotor Blade Heat Transfer Predictions , ASME Paper 94-GT-22 , 1994 .
   Google Scholar
• A. A. Ameri and A. Arnone , Prediction of Turbine Blade Passage Heat Transfer Using a Zero and a Two-Equation Turbulence Model , ASME Paper 94-GT-122 , 1994 .
   Google Scholar
• R. J. Boyle and A. A. Ameri , Grid Orthogonality Effects on Predicted Turbine Midspan Heat Transfer and Performance , ASME Paper 94-GT-123 , 1994 .
   Google Scholar
• R. A. Graziani , M. F. Blair , J. R. Taylor , and R. E. Mayle , An Experimental Study of Endwall and Airfoil Surface Heat Transfer in a Large Scale Turbine Blade Cascade , J. Eng. Power , vol. n102 n, pp. 257 – 267 , 1980 .
   Google Scholar
• A. A. Amer , B. A. Jubran , and M. A. Hamdan , Comparison of Different Two-Equation Turbulence Models for Prediction of Film Cooling from Two Rows of Holes , Numer. Heat Transfer Part A , vol. 21 , pp. 143 – 162 , 1992 .
   Web of Science ®Google Scholar
• S.-W. Kim and T. J. Benson , Calculation of a Circular Jet in Cross Flow with a Multiple-Time-Scale Turbulence Model , Int. J. Heat Mass Transfer , vol. n35 n, pp. 2357 – 2365 , 1992 .
   Google Scholar
• V. K. Garg and R. E. Gaugler , Effect of Velocity and Temperature Distribution at the Hole Exit on Film Cooling of Turbine Blades , ASME Paper 95-GT-2 , 1995 .
   Google Scholar
• A. Jameson , W. Schmidt , and E. Turkel , Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes , AIAA Paper 81 – 1259 , 1981 .
   Google Scholar
• W. Haas , W. Rodi , and B. Schönung , The Influence of Density Difference Between Hot and Coolant Gas on Film Cooling by a Row of Holes Predictions and Experiments, ASME Paper 91-GT-255 , 1991 .
   Google Scholar