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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 |
Modeling of coupled aerogasdynamics and heat transfer processes on the thermal protection surface of a future hypersonic aircraft
Authors: Dimitrienko Yu.I., Zakharov A.A., Koryakov M.N., Syzdykov E.K. | Published: 24.03.2014 |
Published in issue: #3(648)/2014 | |
Category: Calculation and Design of Machinery | |
Keywords: aerogasdynamics, hypersonic aircraft, coupled problems, heat transfer, numerical modeling, TVD scheme, adaptive mesh, thermal protection, ablative beat shield materials. |