Large-Eddy Simulation of Supersonic Combustion in a Mach 2 Cavity Model Scramjet Combustor
Year: 2024
Type: article
Source: AIAA Journal
DOI: 10.2514/1.j064432
Institutions: Lund University, United States Air Force Research Laboratory
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
Awards: G829931388, NAISS
OpenAlex ID: W4404146668
