LEADER 04742nam 22008055 450 001 9910410046403321 005 20210111141532.0 010 $a981-15-3274-5 024 7 $a10.1007/978-981-15-3274-0 035 $a(CKB)4100000011208565 035 $a(MiAaPQ)EBC6178579 035 $a(DE-He213)978-981-15-3274-0 035 $a(PPN)243759932 035 $a(EXLCZ)994100000011208565 100 $a20200418d2020 u| 0 101 0 $aeng 135 $aurcnu|||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aTime-Dependent Mechanical Behavior of Ceramic-Matrix Composites at Elevated Temperatures /$fby Longbiao Li 205 $a1st ed. 2020. 210 1$aSingapore :$cSpringer Singapore :$cImprint: Springer,$d2020. 215 $a1 online resource (373 pages) 225 1 $aAdvanced Ceramics and Composites,$x2662-9305 ;$v1 311 $a981-15-3273-7 327 $aTime-dependent first matrix cracking stress of ceramic-matrix composites at elevated temperatures -- Time-dependent matrix multiple cracking of ceramic-matrix composites at elevated temperatures -- Time-dependent tensile strength of ceramic-matrix composites at elevated temperatures -- Time-dependent tensile behavior of ceramic-matrix composites at elevated temperatures -- Time-dependent fatigue behavior of ceramic-matrix composites at elevated temperatures. 330 $aThis book investigates the time-dependent behavior of fiber-reinforced ceramic-matrix composites (CMCs) at elevated temperatures. The author combines the time-dependent damage mechanisms of interface and fiber oxidation and fracture with the micromechanical approach to establish the relationships between the first matrix cracking stress, matrix multiple cracking evolution, tensile strength, tensile stress-strain curves and tensile fatigue of fiber-reinforced CMCs and time. Then, using damage models of energy balance, the fracture mechanics approach, critical matrix strain energy criterion, Global Load Sharing criterion, and hysteresis loops he determines the first matrix cracking stress, interface debonded length, matrix cracking density, fibers failure probability, tensile strength, tensile stress-strain curves and fatigue hysteresis loops. Lastly, he predicts the time-dependent mechanical behavior of different fiber-reinforced CMCs, i.e., C/SiC and SiC/SiC, using the developed approaches, in order to reduce the failure risk during the operation of aero engines. The book is intended for undergraduate and graduate students who are interested in the mechanical behavior of CMCs, researchers investigating the damage evolution of CMCs at elevated temperatures, and designers responsible for hot-section CMC components in aero engines. . 410 0$aAdvanced Ceramics and Composites,$x2662-9305 ;$v1 606 $aCeramics 606 $aGlass 606 $aComposites (Materials) 606 $aComposite materials 606 $aMechanics 606 $aMechanics, Applied 606 $aMaterials science 606 $aAerospace engineering 606 $aAstronautics 606 $aEngines 606 $aMachinery 606 $aCeramics, Glass, Composites, Natural Materials$3https://scigraph.springernature.com/ontologies/product-market-codes/Z18000 606 $aSolid Mechanics$3https://scigraph.springernature.com/ontologies/product-market-codes/T15010 606 $aCharacterization and Evaluation of Materials$3https://scigraph.springernature.com/ontologies/product-market-codes/Z17000 606 $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050 606 $aEngine Technology$3https://scigraph.springernature.com/ontologies/product-market-codes/T17048 615 0$aCeramics. 615 0$aGlass. 615 0$aComposites (Materials). 615 0$aComposite materials. 615 0$aMechanics. 615 0$aMechanics, Applied. 615 0$aMaterials science. 615 0$aAerospace engineering. 615 0$aAstronautics. 615 0$aEngines. 615 0$aMachinery. 615 14$aCeramics, Glass, Composites, Natural Materials. 615 24$aSolid Mechanics. 615 24$aCharacterization and Evaluation of Materials. 615 24$aAerospace Technology and Astronautics. 615 24$aEngine Technology. 676 $a620.14 700 $aLi$b Longbiao$4aut$4http://id.loc.gov/vocabulary/relators/aut$0769299 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910410046403321 996 $aTime-Dependent Mechanical Behavior of Ceramic-Matrix Composites at Elevated Temperatures$92546839 997 $aUNINA