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Overall Effectiveness for a Film Cooled Turbine Blade Leading Edge With Varying Hole Pitch
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Overall effectiveness, د†, for a simulated turbine blade leading edge was experimentally measured using a model constructed with a relatively high conductivity material selected so that the Biot number of the model matched ...
Thermal Performance Comparisons of Advanced Cooling Designs Under Engine Representative Conditions
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Abstract. Novel turbine blade cooling geometries have conventionally been assessed using computational methods, simplified flat-plate geometries, or large-scale wind tunnel models all at low-technology readiness levels. ...
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