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Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Innovative methodology for calculation and design of liquid-propellant rocket engine combustion chamber

Published: 21.11.2016

Authors: Korotkaya O.V.

Published in issue: #12(60)/2016

DOI: 10.18698/2308-6033-2016-12-1560

Category: Aviation and Rocket-Space Engineering | Chapter: Thermal, Electric Jet Engines, and Power Plants of Aircrafts

    mathematical modeling, finite-element method, substructure, cyclic symmetry, anisotropy coefficients, optimization, mode of deformation, nozzle, combustion chamber, liquid-propellant rocket engine, cooling channels
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