Mathematical simulation of coolant flow in the cooling channel of a liquid rocket engine combustion chamber featuring an extremely high degree of ribbing
Published: 18.11.2019
Authors: Aleksandrenkov V.P., Kovalev K.E., Yagodnikov D.A.
Published in issue: #11(95)/2019
DOI: 10.18698/2308-6033-2019-11-1933
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts