I want to create a micro turbojet engine but i don't know from where I should to begin, so I don't know how calculate the engine shaft mil - the distance between kompressor and turbine, combustion chamber.
need some assistance and references.
Dinesh Kumar Madheswaran
Dear Muhammed Sipahi
You may find this article helpful to you.
https://web.wpi.edu/Pubs/E-project/Available/E-project-032318-100910/unrestricted/MQP_Final_Draft.pdf
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Muhammed Sipahi
Dinesh Kumar Madheswaran thanks for the reference, but i still searching about shaft calculations. I couldn't find it in any reference. some researchers say that it depending on the long of combustion chamber, But it is not enough for me
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