Results 241 to 250 of about 12,641 (263)
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Journal of Engineering for Power, 1977
Experiments have been performed on the film cooling of gas turbine blades in order to study the influence of large temperature differences on the effectiveness of film cooling. A two-dimensional flat plate model was tested in a stream of 1000 K combustion gases flowing at between 110 and 170 m/s. The model was cooled on both sides by jets of air coming
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Experiments have been performed on the film cooling of gas turbine blades in order to study the influence of large temperature differences on the effectiveness of film cooling. A two-dimensional flat plate model was tested in a stream of 1000 K combustion gases flowing at between 110 and 170 m/s. The model was cooled on both sides by jets of air coming
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Transpiration Cooling: Contribution of Film Cooling to the Overall Cooling Effectiveness
International Journal of Turbo and Jet Engines, 1986G.E. Andrews +3 more
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Effect of adverse pressure gradient on film cooling effectiveness
6th Fluid and PlasmaDynamics Conference, 1973V. ZAKKAY, CHI R. WANG, M. MIYAZAWA
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Effects of trench configuration on the film cooling effectiveness of a fan-shaped hole
International Journal of Heat and Mass Transfer, 2021Jae Su Kwak
exaly
Shape optimization of a fan-shaped hole to enhance film-cooling effectiveness
International Journal of Heat and Mass Transfer, 2010Ki-Don Lee, Kwang-Yong Kim
exaly
Film cooling effectiveness: Comparison of adiabatic and conjugate heat transfer CFD models
International Journal of Thermal Sciences, 2009Alain J Kassab, Eduardo Divo
exaly
Improvements of film cooling effectiveness by using Barchan dune shaped ramps
International Journal of Heat and Mass Transfer, 2016Wenwu Zhou, Hui Hu
exaly