LASAUSKAS, Eduardas; LUTZ, Thorsten; DIETZ, Markus. Influence of trailing edge tab on moment characteristics of NACA 23012 airfoil. Aviation, [S. l.], v. 11, n. 4, p. 3–8, 2007. DOI: 10.3846/16487788.2007.9635970. Disponível em: https://journals.vilniustech.lt/index.php/Aviation/article/view/7051. Acesso em: 30 may. 2025.