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Reshaping the Rotor Hub of a 1.5-stage Axial Turbine to Reduce Pressure Losses by a Parametric Groove

Published Online: 2024-10-27

Published Print: 2024-10

Authors

Hayder M. B. Obaida,

Aldo Rona,
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Text and Data Mining valid from 2024-10-01

Version of Record valid from 2024-10-01
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Article History

Received: 4 October 2022

Revised: 17 December 2022

Accepted: 25 January 2023

First Online: 27 October 2024

CONFLICT OF INTEREST

: The authors of this work declare that they have no conflicts of interest.

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