Effects of blade tip clearance on the aerodynamic characteristics and condensation mechanism of internal non-equilibrium condensing flow in vapor centrifugal compressor
Year: 2026
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0314977
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G2038712684, G8513049231
OpenAlex ID: W7148882045
