Titlebook: Design, Fabrication and Testing of Aeroengine Ceramic-Matrix Composite Components; Xiaochong Liu,Longbiao Li Book 2024 The Editor(s) (if a

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High-Temperature Mechanical Properties of Ceramic-Matrix Composites, interlaminar shear strength, in-plane shear strength, flexural strength, cyclic fatigue lifetime, and creep life are obtained from experimental data. The high-temperature mechanical properties can support the engineers to better design CMCs hot-section components.

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2662-9305 aeroengines were also introduced. The book can better help the engineering designers understand the methods used in design and testing of CMC components.978-981-97-6111-1978-981-97-6109-8Series ISSN 2662-9305 Series E-ISSN 2662-9313

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Family Therapy: In and Out of SYNCwere conducted to investigate the damage mechanisms and failure modes. During thermal shock tests, the surface temperature field of the SiC/SiC guide vane was analyzed. The damage characteristics of the single/twin turbine guide vane after experiencing different thermal shocks were discussed.

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Design, Fabrication and Testing of CMC High-Pressure Turbine Guide Vane,were conducted to investigate the damage mechanisms and failure modes. During thermal shock tests, the surface temperature field of the SiC/SiC guide vane was analyzed. The damage characteristics of the single/twin turbine guide vane after experiencing different thermal shocks were discussed.

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Book 2024gines. The book focuses on the design, fabrication and testing of different CMC components, e.g., turbine guide vanes, combustor liner, and turbine blisk, etc. The high-temperature mechanical properties, and performance requirements of the aeroengines were also introduced. The book can better help t

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forms, i.e., three-dimensional four-directional (3D4D) braided, two-dimensional plain-woven (2DPW) and stain woven (2DSW) lamination, are investigated at elevated temperature of 1400 °C. The high-temperature mechanical properties of SiC/SiC composites, e.g., tensile strength, compressional strength,