Hello, hope you are all doing well, I'm starting an internship and as my first task I have been told to analytically model the combustion stability on a combustion chamber in a spacecraft from scratch, but if I'm honest, I do not know where to begin. I do know that that some of the parameters that I have to use are mass flux of my fuel, chamber pressure, injection pressure among others, but I'm stuck at the start due to lack of knowledge, and I was wondering if any of you have some advice for where to begin, be it a book that has the theory of it or anything else, I'm not looking for the solution to the problem because I want to do the project by myself, but I'm lost at where to start.
Thank you all in advance.
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