Hi again Great insights, I'll add some more detail. For the curious, the paper used CFD based simulation with multiple trial-and-error to get those coefficients relating objective function to design variable. Again, I encourage you to drop in a review or two in the future PR for the notebook.
Reg those other articles, I found them interesting but the notebook will get too verbose. I'll do something about them in my blog though :). Fun fact: Sirisha Bandla's hometown,Guntur, isn't very far from mine (like 8 hours or so). S On Mon, Jul 19, 2021 at 8:22 PM Benson Muite <[email protected]> wrote: > Hi Sai, > > It is not immediately clear where the optimization equations come from, > you give references which are great, but may want to see if some of them > explain how the resulting equations are derived from more complicated > models. Probably a few sentences on this are helpful, typically for > studying instabilities, people solve combustion equations that include > fluid mechanics and chemical reactions. A full explanation would > probably take more space than is available, but a few hints would be > helpful. > > Probably also interesting: > > https://en.wikipedia.org/wiki/Indian_Space_Research_Organisation#Launch_vehicles > > Maybe also relevant in the billionaire space race: > > https://www.gulftoday.ae/news/2021/07/19/india-born-woman-helps-design-rocket-that-takes-jeff-bezos-to-space-tomorrow > > Regards, > Benson > > On 7/19/21 5:21 PM, sai_ng wrote: > > Hello Benson > > > > About the background, I suppose you're talking of the "Framing the > > problem" section? The notebook is in alpha stage, I'll be making a > > series of PR to improve it, you could directly review it on the pull > > request :) > > > > Thanks for the link for combustion instability, I will add that as a > > hyperlink reference in the notebook. About the Soyuz model, currently, > > we're only simulating the injector design of a typical rocket agnostic > > of F-1 engine or in this case Soyuz model. This will keep things very > > simple. > > > > Hope I answered your queries. > > > > S > > >
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