Numerical Analysis of a Supercritical Heat Transfer of Cryogenic Methane in Regeneratively Cooled Rocket Engine.

Autor: DJEFFAL, Mohammed Amine1 djeffalmohammed66@gmail.com, BENAMARA, Nabil1, LAHCENE, Abdelkader1, BENOUAR, Ali2, BOULENOUAR, Abdelkader1, MERZOUG, Mohammed1
Zdroj: INCAS Bulletin. Jan-Mar2024, Vol. 16 Issue 1, p33-44. 12p.
Databáze: Academic Search Ultimate