A Film-Cooling CFD Bibliography : 1971-1996

After more than 25 years of three-dimensional film cooling experimental investigations, analytical correlations and modeling, film cooling utilizing computational fluid dynamics has emerged from a similar development-applications growth process into a near-attainable heat transfer engineering tool. Analytical applications include high temperature subsonic to hypersonic flow with complex wall-geometry coolant injection film performance analysis techniques spanning usage from gas turbines to rocket engines to scramjets. In recent years there has been significant development in increased computer power and modeling capacity, increasingly more complex and successful Navier-Stokes turbulence modeling techniques, innovative labor-saving meshing techniques, and more successful validation of experimental results. These combined innovations have continued to transition computational film cooling technology from the academic, government and commercial research and development environment to the industrial design-analysis environment. This bibliography is an openliterature reference resource whose papers collectively describe the continual emerging of numerical film cooling as a viable design tool for high temperature components.


Acknowledgment
A special thanks and appreciation is extended to Ms. Sandra Moltz of the GE Aircraft Engines Lynn library for her assistance in this research.Without the outstanding resources of the GEAE and MIT library systems, the extent of this bibliography would not have been possible.

E EN NE ER RG GY Y M MA AT TE ER RI IA AL LS S Materials Science & Engineering for Energy Systems
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Beeck, A.,1992.Flow Field Investigations into    the Aerodynamic Behavior of a Highly Loaded Turbine Cascade with Cooling Air Injection at the Leading Edge, Ph.D. Thesis, University of the Federal Armed Forces, Munich (in German).Beeck, A., Fottner, L., Benz, E. and Wittig, S., 1993.The Aerodynamic Effect of Coolant Ejection in the Leading Edge Region of a Film-Cooled Turbine Blade, Heat Transfer and Cooling in Gas Turbines, AGARD-CP-527, Paper No. 35.Befrui, B.A., 1994.Turbulence Modeling Needs of Commercial CFD Codes: Complex Flows in the Aerospace and Automotive Industries, Industry- Wide Workshop on Computational Turbulence Modeling, NASA CP-10165, pp.171-192.Benz, E. and Wittig, S., 1992.Prediction of the Interaction of Coolant Ejection with the Main Stream at the Leading Edge of a Turbine Blade: Attached Grid Application, Proceedings of the International Symposium Heat Transfer in Turbo- machinery, Athens.
1993.Analysis of Cooling Jets near the Leading Edge of Turbine Blades, Computational and D.M. KERCHER Zhou, J.-M., 1994.A Computational and Experi- mental Investigation of Gas Turbine Blade Film Cooling, Ph.D. Thesis, University of British Columbia.Zhou, J.-M., Salcudean, M. and Gartshore, I.S., 1994.Application of the Multiple-Time-Scale Turbulence Model to the Prediction of 2-D Film Cooling Effectiveness, Heat Transfer 1994 Proceedings of the lOth International Heat Transfer Conference, Vol. 3, G.F. Hewitt (ed.), Paper No.4-EC-27, pp.125-130.

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