Simulation Study of Gas Cooling for Aero-Engine Borescope Probes
After an aero-engine shuts down, the high temperature within the core flow path prevents conventional borescope probes from performing immediate internal inspections due to their limited thermal resistance, thereby constraining rapid turnaround capabilities for aircraft. To address this challenge, t...
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| Prif Awduron: | , , , , |
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| Fformat: | Artigo |
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MDPI AG
2025-09-01
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| Cyfres: | Aerospace |
| Pynciau: | |
| Mynediad Ar-lein: | https://www.mdpi.com/2226-4310/12/9/852 |
| Tagiau: |
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