Influence of Spike-Nosed Length on Aerodynamic Drag of a Wing-Projectile Model . Advances in Military Technology, [S. l.], v. 17, n. 1, p. 33–45, 2022. DOI: 10.3849/aimt.01542. Disponível em: https://www.aimt.cz/index.php/aimt/article/view/1542.. Acesso em: 6 may. 2024.