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- W4295278320 abstract "Abstract FGM is a special class of composite material that was first developed in Japan around 1984 for the propulsion system and airframe of space planes. The challenge was to create a thermal barrier that would be capable of withstanding a temperature of 1000 °C over a cross-section of 10 mm. A sharp interface between the matrix and the reinforcement in a traditional composite material would cause cracking in high temperatures. The cracks occur due to the generation of interfacial stress induced by the mismatch of thermal expansion between two different materials." @default.
- W4295278320 created "2022-09-12" @default.
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- W4295278320 date "2022-01-01" @default.
- W4295278320 modified "2023-09-26" @default.
- W4295278320 title "Development of FGM and FGAM" @default.
- W4295278320 cites W2055550171 @default.
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- W4295278320 doi "https://doi.org/10.1007/978-3-031-05863-9_8" @default.
- W4295278320 hasPublicationYear "2022" @default.
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