Secondary Loss Reduction via Integrated Endwall and Blade Profiling in Turbine Stage
Year: 2026
Type: article
Source: Journal of Propulsion and Power
DOI: 10.2514/1.b40271
Institution: Harbin Institute of Technology
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W7204116796
