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RISBoundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The focus of this article is the impact of surface roughness on the boundary layer caused by a 7YSZ thermal barrier coating (TBC). Experimental investigations are conducted on a NGV installed inside the wind tunnel for ...
Wind Tunnel Testing at TRL4 of EBC-Coated SIC/SIC Nozzle Guide Vanes for High-Pressure Turbines With Trailing Edge Cooling
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Abstract. To fulfill the high flight requirements for a significantly lower environmental impact, new approaches to the design of engines are required. One solution to build an engine as a whole more efficiently is the use ...
Assessment of Computational Fluid Dynamic Modeling of Multi-Jet Impingement Cooling and Validation With the Experiments
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The current study involves numerical and experimental investigations of circular in-line jets impinging on a heated flat plate. The generic configuration is characterized by nine jets, each with a diameter of D = 0.0152 ...