Mathematical Models of Transonic Flatter of Aerody-namic Control Surfaces of Supersonic Aircraft. Advances in Military Technology, [S. l.], v. 17, n. 2, p. 195–209, 2022. DOI: 10.3849/aimt.01543. Disponível em: https://www.aimt.cz/index.php/aimt/article/view/1543.. Acesso em: 3 may. 2024.