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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