DEVELOPMENT OF A MATHEMATICAL MODEL FOR THE COOLING CHANNEL OF A LIQUID PROPELLANT ROCKET ENGINE'S CHAMBER WITH RESPECT FOR …
V Sliusariev, V Bucharskyi - Eastern-European Journal of …, 2024 - search.ebscohost.com
This study focuses on the processes occurring within the cooling channels of a liquid rocket
engine chamber. It is important to note that, from a design-stage efficiency prediction …
engine chamber. It is important to note that, from a design-stage efficiency prediction …
Mathematical model for heat transfer in variable thickness fins for rocket engines
V Sliusariev, V Bucharskyi - Challenges and Issues of Modern …, 2024 - cims.fti.dp.ua
Purpose. This article aims to develop a mathematical model for a fin in the cooling system of
liquid propellant rocket engines. The objective is to enable calculations for fins with arbitrary …
liquid propellant rocket engines. The objective is to enable calculations for fins with arbitrary …