A Computational Study of the NASA High-Lift Common Research Model Using OVERFLOW on an Overset Mesh
Year: 2022
Type: conference-paper
Source: AIAA AVIATION Forum
DOI: 10.2514/6.2022-3592
Institution: Boeing (United States)
Language: English
Subfield: Computational Mechanics
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4283218113
