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Investigating the thermohydraulic efficiency of the liquid-propellant rocket engine porous tract of cooling with the interchannel coolant flow
Authors: Anfimov M.V. | Published: 17.10.2017 |
Published in issue: #10(15)/2017 | |
DOI: DOI: 10.18698/2541-8009-2017-10-188 | |
Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
Keywords: Thermohydraulic efficiency, porous tract, liquid-propellant rocket engine cooling, thermal protection |