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Design of a Heat Transfer Intensification System for Hydrocarbon Fuel in the Cooling Channels of the Liquid Rocket Engine
Authors: Yusha V.L., Chernov G.I., Shcherban K.V. | Published: 06.09.2018 |
Published in issue: #8(701)/2018 | |
Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
Keywords: liquid rocket engine, strength analysis, thermal analysis, hypersonic aircraft, cooling system, heat transfer intensification systems |