Effect of Upstream Wake on Shower-Head Film Cooling by Ping-Hei Chen, Jr-Ming Miao

“…The present study aims to investigate the effect of an upstream wake on the convective transport phenomena over a turbine blade with shower-head film cooling. A naphthalene sublimation technique was implemented to obtain the detailed mass transfer distributions on both suction and pressure surfaces of the test blade. …”
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A Film-Cooling CFD Bibliography: 1971–1996 by D. M. Kercher

“…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. …”
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Mass Transfer over a Film-Cooled Turbine Blade by Ping-Hei Chen, Jr-Ming Miao

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Turbine Airfoil Leading Edge Film Cooling Bibliography: 1972–1998 by D. M. Kercher

Subjects: “…Film cooling…”
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Experimental Film Cooling Effectiveness of Three-Hole-Branch Circular Holes by Fan Yang, Mohammad E. Taslim

“…A three-hole-branch geometry for film cooling is proposed. Each branch is made up of a streamwise 30°-angled circular hole with a circular hole of the same diameter on each side of it. …”
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Film Cooling from a Single Row of Compound Angle Holes at High Blowing Ratios by Phillip M. Ligrani, Joon Sik Lee

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Film Cooling Effectiveness Data for Simple Injection Geometries: A Collection of Three-Axis Plots by L. D. Stone, R. J. Goldstein

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Film Cooling Optimization Using Numerical Computation of the Compressible Viscous Flow Equations and Simplex Algorithm by Ahmed M. Elsayed, Farouk M. Owis, M. Madbouli Abdel Rahman

“…Film cooling is vital to gas turbine blades to protect them from high temperatures and hence high thermal stresses. …”
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Experimental Study of Two Rows Hybrid Film Cooling Holes Over Flat Plate Surface Using IR Technology by Ahmed A. Naji, Harbi A. Daud, Nabil J. Yasin, Ahmed A. Jasim

“… The study examines the effectiveness of two rows of hybrid film cooling holes over a plate surface using infrared technology and a thermal wind tunnel. …”
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Detailed Film Cooling Measurements over a Gas Turbine Blade Using a Transient Liquid Crystal Image Technique by Hui Du, Srinath V. Ekkad, Je-Chin Han, C. Pang Lee

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Adiabatic Effectiveness and Heat Transfer Coefficient of Shaped Film Cooling Holes on a Scaled Guide Vane Pressure Side Model by Jan Dittmar, Achmed Schulz, Sigmar Wittig

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Effect of Turbulence Intensity on Cross-Injection Film Cooling at a Stepped or Smooth Endwall of a Gas Turbine Vane Passage by Pey-Shey Wu, Shen-Ta Tsai, Yue-Hua Jhuo

“…This study is concerned with a film cooling technique applicable to the protection of the endwalls of a gas turbine vane. …”
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Numerical study on the effect of rim seal slot filleting on turbine endwall cooling by Xinchun Li, Na Wei, Liuliu Shi, Eryun Chen

“…In this study, the effect of rim seal slot filleting on turbine endwall film cooling performance is numerically investigated. …”
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Recent Studies in Turbine Blade Cooling by Je-Chin Han

“…This presentation includes unsteady high free-stream turbulence effects on film cooling performance with a discussion of detailed heat transfer coef- ficient and film-cooling effectiveness distributions for standard and shaped film-hole geometry using the newly developed transient liquid crystal image method.…”
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An Experimental Investigation on Transpiration Cooling Part II: Comparison of Cooling Methods and Media by J. H. Wang, J. Messner, H. Stetter

“…The natures of transpiration cooling and film cooling including leading and trailing edge injection cooling were compared. …”
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Film Effectiveness Downstream the Trenches with Tilted Target Wall by Fan Yang, Mohammad E. Taslim

“…Film cooling is a commonly-accepted effective way to protect the gas turbine hot sections from the high temperature products of the combustion chamber. …”
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Extreme thermal load generation method for high-temperature structures in atmospheric environment by WANG Binwen, ZHANG Yi, QIN Qiang, CHEN Hong, WU Jingtao

“…Secondly, a method of creating closed transparent environment for graphite heating elements has been developed, with double-layer gas film cooling, which avoids severe oxidation of graphite heating elements in contact with oxygen at high temperatures and achieves the application of large heat flux loads in the atmospheric environment. …”
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