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