KUMAR, A.; PANDA, H. S.; BISWAL, T. K.; APPAVURAJ, R. Flow Around a Conical Nose with Rounded Tail Projectile for Subsonic, Transonic, and Supersonic Flow Regimes : A Numerical Study. Defence Science Journal, [S. l.], v. 64, n. 6, p. 509–516, 2014. DOI: 10.14429/dsj.64.8111. Disponível em: https://publications.drdo.gov.in/ojs/index.php/dsj/article/view/8111. Acesso em: 3 jul. 2025.