Unstarting/starting characteristics of supersonic inlet investigated by wind tunnel test and Reynolds-stress-compensated scale-adaptive simulation
Year: 2026
Type: article
Source: Physics of Fluids
DOI: 10.1063/5.0316018
Institution: Nanjing University of Aeronautics and Astronautics
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G4256237707, G6711464958
OpenAlex ID: W7128599940
