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...

Full description

Bibliographic Details
Main Authors: Mario Carta, Tiziano Ghisu, Shahrokh Shahpar
Format: Article
Language:English
Published: MDPI AG 2023-08-01
Series:International Journal of Turbomachinery, Propulsion and Power
Subjects:
Online Access:https://www.mdpi.com/2504-186X/8/3/24