Reshaping the Rotor Hub of a 1.5-stage Axial Turbine to Reduce Pressure Losses by a Parametric Groove
Year: 2024
Type: article
Source: Thermal Engineering
Authors: Hayder M. B. Obaida, Aldo Rona
Institutions: Middle Technical University, University of Leicester
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4403844395
