The Generalized Tensor Model for Numerical Investigation of Combustion and Flow Processes in Liquid Rocket Engine Chamber

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...

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Bibliographic Details
Main Authors: Nijat Abdulla, Parviz Abdullayev
Format: Article
Language:English
Published: Turkish Air Force Academy 2023-01-01
Series:Havacılık ve Uzay Teknolojileri Dergisi
Subjects:
liquid rocket engine
combustion and flow processes
generalized tensor model
Online Access:https://jast.hho.msu.edu.tr/index.php/JAST/article/view/514/374

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