R. C. MEHTA. Numerical Flowfield Visualization Over Heat Shield Of Satellite Launch Vehicle at Mach 0.8 - 3.0. Journal of Aerospace Sciences and Technologies, [S. l.], v. 63, n. 3, p. 183–193, 2023. DOI: 10.61653/joast.v63i3.2011.544. Disponível em: http://joast.org/index.php/joast/article/view/544. Acesso em: 18 oct. 2024.