CHIDAMBARAM, P. K.; KUMAR, A. Combined Effect of Diaphragm and Oxidizer Swirl on Regression Rate in Hybrid Rocket Motors. Defence Science Journal, [S. l.], v. 64, n. 1, p. 21–26, 2014. DOI: 10.14429/dsj.64.3770. Disponível em: https://publications.drdo.gov.in/ojs/index.php/dsj/article/view/3770. Acesso em: 3 aug. 2025.