Control of incident shock wave/boundary layer interaction by concave surface
Year: 2025
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0288609
Institution: Nanjing University of Aeronautics and Astronautics
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G1385089591, G6336693799
OpenAlex ID: W4413952760