Stall mechanisms of a transonic compressor rotor with axisymmetric and nonaxisymmetric tip clearance layouts
Year: 2025
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0258043
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4408448566
