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Influence of Heat Exchange Intensity in the Rocket Thrust Chamber on the Cooling Channel Efficiency
| Authors: Aleksandrenkov V.P. | Published: 03.08.2017 |
| Published in issue: #4(115)/2017 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts | |
| Keywords: annular channel, intensification of convective heat transfer, thermal and hydraulic efficiency and characteristics, maximum heat dissipation, heat transfer coefficients ratio, limiting efficiency | |