Abstract
The aim of this paper is to compare various mathematical models simulating the turbulent flow in a solid propellant rocket engine. For comparison, the most frequently used models were chosen for simulations of flow in the S5 rocket engine. For this type of engine experimental data are available allowing comparison of the simulations with reality. The LES Smagorinsky model provided the best results, while type RANS models appeared to be less suitable for this task.
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callSimilar Papers
More From: Advances in Military Technology
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
