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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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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

    liquid rocket engine, cooling channel, extremely high degree of ribbing, heat transfer, mathematical model
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