The Generalized Tensor Model for Numerical Investigation of Combustion and Flow Processes in Liquid Rocket Engine Chamber
Combustion and flow thermogasdynamics is one of the most sophisticated computational stages in liquid rocket engine (LRE) design. A considerable amount of different methodologies used to conduct the thermogasdynamic analysis of the combustion and flow process and...
Main Authors: | Nijat Abdulla, Parviz Abdullayev |
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Format: | Article |
Language: | English |
Published: |
Turkish Air Force Academy
2023-01-01
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Series: | Havacılık ve Uzay Teknolojileri Dergisi |
Subjects: | |
Online Access: | https://jast.hho.msu.edu.tr/index.php/JAST/article/view/514/374 |
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