HOST turbine heat transfer program summary

The objectives of the HOST Turbine Heat Transfer subproject were to obtain a better understanding of the physics of the aerothermodynamic phenomena and to assess and improve the analytical methods used to predict the flow and heat transfer in high temperature gas turbines. At the time the HOST project was initiated, an across-the-board improvement in turbine design technology was needed. A building-block approach was utilized and the research ranged from the study of fundamental phenomena and modeling to experiments in simulated real engine environments. Experimental research accounted for approximately 75 percent of the funding with the remainder going to analytical efforts. A healthy government/industry/university partnership, with industry providing almost half of the research, was created to advance the turbine heat transfer design technology base.

[1]  R. P. Dring,et al.  The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model. Part 4: Aerodynamic data tabulation , 1987 .

[2]  Suhas V. Patankar,et al.  Prediction of transition on a flat plate under the influence of free-stream turbulence using low-Reynolds-number two-equation turbulence models , 1987 .

[3]  D. E. Metzger,et al.  Heat transfer in shrouded rectangular cavities , 1986 .

[4]  R. P. Dring,et al.  The Effects of Turbulence and Stator/Rotor Interactions on Turbine Heat Transfer: Part I—Design Operating Conditions , 1988 .

[5]  R. P. Dring,et al.  The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model. Volume 2: Heat transfer data tabulation. 15 percent axial spacing , 1986 .

[6]  L. W. Florschuetz,et al.  Flow Distributions and Discharge Coefficient Effects for Jet Array Impingement With Initial Crossflow , 1982 .

[7]  L. D. Hylton,et al.  Measurements of Heat Transfer Distribution Over the Surfaces of Highly Loaded Turbine Nozzle Guide Vanes , 1984 .

[8]  D. R. Richards,et al.  Forced convection heat transfer to air/water vapor mixtures , 1984 .

[9]  M. S. Mihelc,et al.  Analytical and Experimental Evaluation of the Heat Transfer Distribution over the Surfaces of Turbine Vanes , 1983 .

[10]  L. W. Florschuetz,et al.  Jet array impingement flow distributions and heat transfer characteristics. Effects of initial crossflow and nonuniform array geometry. [gas turbine engine component cooling] , 1982 .

[11]  R. P. Dring,et al.  The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer of a large-scale rotating turbine model, volume 1 , 1987 .

[12]  Application of CFD codes to the design and development of propulsion systems , 1987 .

[13]  Herbert J. Gladden,et al.  Heat Transfer Results and Operational Characteristics of the NASA Lewis Research Center Hot Section Cascade Test Facility , 1985 .

[14]  M. E. Crawford,et al.  STAN5: A program for numerical computation of two-dimensional internal and external boundary layer flows , 1976 .

[15]  F. S. Stepka Analysis of uncertainties in turbine metal temperature predictions , 1980 .

[16]  P. D. Thomas Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles, theory , 1979 .