Browsing by Subject "Film-Cooling"
Now showing items 1-2 of 2
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(2012-10-19)In this study, the film-cooling effectiveness in different regions of gas turbine blades was investigated with various film hole/slot configurations and mainstream flow conditions. The study consisted of three parts: 1) ...
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(2018-07-27)The flow around a gas turbine blade is inherently three-dimensional and based on the Re-number and the blade geometry, it may be laminar, transitional or turbulent. The blade surfaces are subject to periodic unsteady wakes ...