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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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Wedi'i Gadw mewn:
Manylion Llyfryddiaeth
Prif Awduron: Lu Jia, Hao Zeng, Rui Xi, Jingbo Peng, Xinyao Hou
Fformat: Artigo
Iaith:Inglês
Cyhoeddwyd: MDPI AG 2025-09-01
Cyfres:Aerospace
Pynciau:
Mynediad Ar-lein:https://www.mdpi.com/2226-4310/12/9/852
Tagiau: Ychwanegu Tag
Dim Tagiau, Byddwch y cyntaf i dagio'r cofnod hwn!