All articles by "Korotkaya O.V."

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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

Application of the substructure method for thermal stress-strain assessment of a liquid-propellant rocket engine combustion chamber

Published: 08.10.2013

Authors: Gavrushin S.S., Krasnovskiy E.E., Korotkaya O.V., Strizhenko P.P., Katkov R.E.

Published in issue: #4(16)/2013

DOI: 10.18698/2308-6033-2013-4-705

Category: Engineering | Chapter: Rocket and space technology

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