Direct numerical simulation of boundary layer transition induced by roughness element in a low Reynolds number compressor blade
Year: 2024
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0239694
Institution: Xi'an Jiaotong University
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Award: G6200535338
OpenAlex ID: W4404993193