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    Boundary Layer Analysis of a Transonic High-Pressure Turbine Vane Using Ultra-Fast-Response Temperature-Sensitive Paint 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 009:;page 91013-1
    Author(s): Petersen, Anna; Hilfer, Michael
    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 ...
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    Design and Manufacture of SiC/SiC Nozzle Guide Vanes With Environmental Barrier Coatings for High-Pressure Turbines 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 002:;page 21021-1
    Author(s): Süß, Fabia; Schöffler, Robin; Friedrich, Lion; Petersen, Anna; Vogel, Felix; Frieß, Martin; Ebach-Stahl, Andrea
    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 ...
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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