Thermal computational fluid dynamics analysis of a converging-diverging rocket nozzle at varying inlet temperatures using k-w Turbulence Model. Natural and Applied Sciences International Journal (NASIJ), Peshawar, Pakistan, v. 7, n. 1, p. 104–121, 2026. DOI: 10.47264/idea.nasij/7.1.6. Disponível em: https://ideapublishers.org/index.php/nasij/article/view/7.1.6. Acesso em: 6 sep. 2026.