Numerical simulation of combustion in the chamberof a model low-thrust rocket engine operating on the gaseous oxygen–methane components
Published: 20.07.2023
Authors: Fedotova K.V., Kovalev K.E., Vorozheeva O.A.
Published in issue: #7(139)/2023
DOI: 10.18698/2308-6033-2023-7-2292
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts