Simulation and Experimental Study of Gas Turbine Blade Tenon-Root Detachment on Spin Test
This paper addresses the critical issue of turbine blade containment in aircraft engines, crucial for ensuring flight safety. Through a comprehensive approach integrating numerical simulations and experimental validations, the containment capabilities of gas turbine engine casings are thoroughly ana...
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| Hauptverfasser: | , , , , , |
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| Format: | Artigo |
| Sprache: | Inglês |
| Veröffentlicht: |
MDPI AG
2024-08-01
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| Schriftenreihe: | Aerospace |
| Schlagworte: | |
| Online-Zugang: | https://www.mdpi.com/2226-4310/11/8/629 |
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