Fluid-structural interaction for turbine blade rib models
Aircraft turbine blades experience high stresses and temperatures within engine turbines during flight. Over time, the blade structure undergoes deformation, leading to a phenomenon known as creep. Eventually, the blade structure would fail and crack, necessitating for a replacement. An aircraft wou...
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| Format: | Final Year Project |
| Language: | English |
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Nanyang Technological University
2024
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| Online Access: | https://hdl.handle.net/10356/177306 |
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| Institution: | Nanyang Technological University |
| Language: | English |