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Calculation of screw lines of the shell for cooling combustion chambers of liquid rocket engines
| Authors: Ustinov K.A., Ryazantsev A.Yu., Bataronov I.L. | Published: 21.09.2026 |
| Published in issue: #10(799)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: liquid rocket engine, cooling channels, combustion chamber, cooling path |
The Application of Cyclic Symmetry and the Substructure Method in the Thermal Stress Analysis of the Combustion Chamber of the Liquid-Propellant Rocket Engine with LOX Cooling
| Authors: Korotkaya O.V., Gavryushin S.S. | Published: 20.01.2016 |
| Published in issue: #1(670)/2016 | |
| Category: Technology and Process Machines | |
| Keywords: mathematical modeling, finite element method, substructure, cyclic symmetry, stress-strain state, nozzle, combustion chamber, liquid-propellant rocket engine, cooling channels, LOX-cooling |