The loss mechanisms and vortex dynamics of rotor platform step geometries in a low-speed research compressor stage
Year: 2024
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0221380
Institution: Shanghai Jiao Tong University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4401595485
