[mlpack] Rocket injector demo

[Benson Muite]

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
>