Introduction:

The practical course centers around two key components. Initially, participants acquire proficiency in using CFD tools to simulate rocket engines, enabling them to predict the outcomes associated with different models. To support this, sensitivity analyses are conducted, allowing participants to evaluate the uncertainty of the results generated. Secondly, participants engage in the physical evaluation of the results obtained. This involves comprehensive discussions of the findings, utilizing a range of analytical tools for in-depth analysis.

Objective:

Utilize CFD methods to model intricate physical processes. Specifically, participants will gain the ability to forecast turbulent combustion in spacecraft engines using cost-effective approaches. They will also learn to differentiate between various numerical models and make independent selections among them. Additionally, they will analyze interrelated phenomena and derive conclusions from their findings. Lastly, participants will be equipped to perform independent expert evaluations on innovative designs of rocket combustion chambers.

Teaching and learning method:

At the beginning, participants undergo a comprehensive training program. They start by receiving instructional materials, which include presentation scripts covering the theory of turbulent combustion. The theoretical concepts are presented in lectures. Practical application of numerical tools is emphasized in tutorials. Throughout the training course, specific milestones are established for the participants’ projects, and the results are reviewed collectively.