Heat Transfer Analysis of Damaged Shrouded High-Pressure Turbine Rotor Blades
Due to the increasingly high turbine inlet temperatures, heat transfer analysis is now, more than ever, a vital part of the design and optimization of high-pressure turbine rotor blades of a modern jet engine. The present study aimed to find out how shape deviation and in-service deterioration affec...
Main Authors: | , , |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-08-01
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Series: | International Journal of Turbomachinery, Propulsion and Power |
Subjects: | |
Online Access: | https://www.mdpi.com/2504-186X/8/3/24 |