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Experimental Investigations of Platform Film-Cooling in Highly-Loaded Turbine Vanes formatIsbn:Softcover - 9783944331362 Zum Teil werden auch hier

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Experimental Investigations of Platform Film-Cooling in Highly-Loaded Turbine Vanes formatIsbn:Softcover - 9783944331362 Zum Teil werden auch hierIn modern gas turbines, the airfoil platforms in the high pressure turbine are subject to extreme aerodynamic and thermal loads. Hence, these surfaces are extensively cooled using film cooling as key technology. The coolant is injected through small holes into the wall boundary layer which is of three dimensional and highly turbulent character. It is further influenced by a set of secondary flow vortices which are driven by the lateral pressure

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