Investigating and experimentally determining the characteristics of thermal-hydraulic processes in the cooling channels of liquid rocket engine combustion chambers featuring an extremely high degree of ribbing
Published: 12.12.2017
Authors: Aleksandrenkov V.P., Kovalev K.E., Yagodnikov D.A.
Published in issue: #12(72)/2017
DOI: 10.18698/2308-6033-2017-12-1710
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts