The numerical modelling of processes in combustion chambers of low thrust rocket engines

Abstract


The mathematical model of processes in combustion chambers of low trust rocket engines with diphasic fuel compositions and results of calculations of the chamber of the engine with fuel composition gaseous oxygen / ethanol are presented.


About the authors

V. L. Salich

Institute of Mechanical Engineering

Author for correspondence.
Email: salich_vas@mail.ru

Russian Federation

candidate of technical science
leading research engineer, head of research division

References

Statistics

Views

Abstract - 46

PDF (Russian) - 16

Article Metrics

Metrics Loading ...

PlumX

Dimensions

Refbacks

  • There are currently no refbacks.

Copyright (c) 2019 VESTNIK of Samara University. Aerospace and Mechanical Engineering

License URL: https://journals.ssau.ru/index.php/vestnik/about/editorialPolicies#custom-2

This website uses cookies

You consent to our cookies if you continue to use our website.

About Cookies