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RISDevelopment of 1400 °C (2552 °F) Class Ceramic Matrix Composite Turbine Shroud and Demonstration Test With JAXA F7 Aircraft Engine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The authors developed 1400 °C (2552 °F) class ceramic matrix composite (CMC) material system, which consists of silicon carbide (SiC) fibers and SiC matrix and ytterbium silicate base matrix, aiming for higher temperature ...