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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 ...
Design and Manufacture of SiC/SiC Nozzle Guide Vanes With Environmental Barrier Coatings for High-Pressure Turbines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Increasing the efficiency of jet engines is essential to meet the demanded climate targets. Ceramic matrix composites (CMCs) are strong candidates for aircraft applications because they withstand high temperatures, while ...
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 ...