Aerodynamic Effect of Artificial Ice Shapes on the 5.2% Scale Semispan High-Lift Common Research Model in the NASA National Transonic Facility
Year: 2025
Type: conference-paper
DOI: 10.2514/6.2025-3463
Institutions: Glenn Research Center, Boeing (United States)
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4412486756
