Simulating working bodies in the mixer of a low-thrust liquid propellant rocket engine with a thrust of 10 to 15 N: comparing three models of flow and mixing based on solving Reynolds-averaged Navier — Stokes equations
Published: 08.02.2021
Authors: Semkin E.V.
Published in issue: #2(110)/2021
DOI: 10.18698/2308-6033-2021-2-2057
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts