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Study of Hydraulic Characteristics of the Cooling Path of a Model Liquid Rocket Engine Manufactured using Additive Technology of Selective Laser Melting
| Authors: Yagodnikov D.A., Aleksandrenkov V.P., Kovalev K.E., Grigoryants A.G., Drenin A.A. | Published: 20.12.2019 |
| Published in issue: #6(129)/2019 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: hydraulic characteristics, cooling path, combustion chamber fins, additive technologies, thermal protection | |