Study on continuous incident compression waves/turbulent boundary layer interaction under the influence of an expansion corner
Year: 2025
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0306660
Institution: Nanjing University of Aeronautics and Astronautics
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4417433747
