An aerodynamic investigation of a high-pressure turbine using rotor casing static pressure measurements at engine representative conditions with different tip designs, tip gaps, and inlet temperature profiles
A rotating high-pressure (HP) turbine, in modern aircraft engines, is subjected to high cyclic thermal and mechanical loads. Shroudless turbines experience high heat loads on the rotor tip and casing, which makes them one of the life-limiting components of an engine. If the rotor tip starts to erode...
Main Authors: | , , , , , , , |
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Format: | Journal article |
Language: | English |
Published: |
American Society of Mechanical Engineers
2025
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