A Novel Cooling Design and Improvement of a Radial-Inflow Turbine Rotor Blade
Year: 2025
Type: article
Source: Journal of Turbomachinery
DOI: 10.1115/1.4070460
Institution: Harbin Institute of Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Award: G7566638924
OpenAlex ID: W4416579107