On understanding the material removal mechanism when cutting Ceramic Matrix Composites (CMCs)
The continuous increase in Turbine Entry Temperature (TET) in aerospace gas-turbines is the main driving force behind research efforts in the development of Ceramic Matrix Composites CMCs. Among different ceramic composites, SiC-based \CMCs are the material choice for aero-engine manufacturers for...
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| Format: | Thesis (University of Nottingham only) |
| Language: | English English |
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2018
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| Online Access: | https://eprints.nottingham.ac.uk/55445/ |