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Hydrogen fuel rocket engines simulation using LOGOS code
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DOI：10.1016/j.ijhydene.2014.04.150.png)
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Abstract
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Computer aided design of new effective and clean hydrogen rocket engines needs mathematical tools for supercomputer modeling of hydrogen oxygen components mixing and chemically reacting in rocket combustion chambers. The paper presents the results of computer code developing, verification and validation, making it possible to simulate unsteady processes of ignition and combustion of hydrogen fuel in rocket engines. Restrictions on unsteady gas dynamics working cycles supercomputer simulations due to accumulations of errors are developed. Copyright (C) 2014, Hydrogen Energy Publications, LLC. Published by Elsevier Ltd. All rights reserved.
Keywords:
Combustion
Ignition
Engine
Diffusion
Turbulence
Mathematical simulation
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