1.
Kumar A, Panda H, Biswal T, Appavuraj R. Flow Around a Conical Nose with Rounded Tail Projectile for Subsonic, Transonic, and Supersonic Flow Regimes : A Numerical Study. DSJ [Internet]. 1Nov.2014 [cited 3Apr.2020];64(6):509-16. Available from: https://publications.drdo.gov.in/ojs/index.php/dsj/article/view/8111