I would like to design and eventually build a small axial turbine jet. I plan on it being between the size of a coffe thermos and a 2 liter pop bottle. I am undecided on the fuel but am open to anything including propane, alcohol, gas (possibly others i can't think of?). I plan on doing this the right way from start to finish. I want to work my way through all the math to figure out exactly what I am doing, and make 3d and CAD mock ups as I go. I suppose I should start by experimenting (mathematically) with the combustion chamber, which takes up about/less than a quarter of the size (if i'm not mistaken), and draw up a chart of provided kinetic energy for all the possible fuels versus the possible target sizes. Then try and work that out as to the turbine and compressor design accounting for aerodynamics and weight versus the required airflow.
Is this the right way to go about it? Where do I look to find the formulas for calculating this? Are there any good books that you can recommend? any help is greatly appreciated and i can't wait to get my calculator going!
