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http://bura.brunel.ac.uk/handle/2438/32430| Title: | Development of FGM and FGAM |
| Authors: | Pei, E Kabir, I |
| Issue Date: | 13-Sep-2022 |
| Publisher: | Springer |
| Citation: | Pei, E. and Kabir, I. (2022) 'Development of FGM and FGAM', in D. Godec et al. (eds.) A Guide to Additive Manufacturing (Springer Tracts in Additive Manufacturing (STAM); Part F3252), 2022, Part F3252). Cham, Springer, pp. 307 - 319. doi: 10.1007/978-3-031-05863-9_8. |
| Series/Report no.: | Springer Tracts in Additive Manufacturing;Part F3252 |
| 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. |
| URI: | https://bura.brunel.ac.uk/handle/2438/32430 |
| DOI: | https://doi.org/10.1007/978-3-031-05863-9_8 |
| ISBN: | 978-3-031-05862-2 (pbk) 978-3-031-05863-9 (ebk) |
| Other Identifiers: | ORCiD: Eujin Pei https://orcid.org/0000-0002-3628-8689 Chapter 8 |
| Appears in Collections: | Brunel Design School Research Papers |
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