The effects of optimized rim seal geometry on the end wall flow of a high-lift low-pressure turbine
Year: 2025
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0254037
Institution: Civil Aviation University of China
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Award: G8653487096
OpenAlex ID: W4408102674