I'm making pic related, I could use some help.
1. I have a smaller flametube diameter than the calculated one, Can I compensate that by drilling larger holes?
2. Where should the holes be positioned?
3. I want to use gasoline, so do I go with pump or a pressurized container?
4.how do I make an injector that aerosolizes the fuel?
The calculator I used,
http://www.nuclearprojects.com/jetspecs/flametube.php
>>1216361
I can answer no.3 for you and you do not want a large canister of pressurized gasoline anywhere near you or your property, and especially not anywhere near a turbojet engine in operation. Use a high-pressure fuel pump and have a smaller canister closer to the nozzle that you can pressurize to give some extra startup juice
I really don't know about the hole/chamber ratio.
But
>>1216365
Has the right idea. A high pressure fuel pump connected to a "hydropneumatic" chamber can assure a steady pressurized flow. There are injectors that aereolize the fuel, they have nozzles like atomizers. It would be helpful if you could have a small presurrized air pipe going paralel to the injecror, so the fuel get's air directly. Or a pre-oxidation chamber. I understand that this is not what the jet is for, but it would help to make combustion more efficient.
Also, are you building a generator? Or do you want Thrust?
>>1216365
Thanks anon. I thought I couldn't get a decent flow rate without using beefy pumps.
>>1216554
> A high pressure fuel pump connected to a "hydropneumatic" chamber
Wouldn't that cost a fortue to make/build?
>air pipe paralel to the injector
Yeah, I'm pumping air directly to the combustion chamber till the turbo self sustains.
Also, I want thrust. I'm not pushing anything with it, but I want to measure thrust, temp, pressure and rippums of the turbo.
>>1216361
Wtf is the diameter and what are you doing with the waste heat? And DIY? There's a reason cars, gasoline generators, and small planes don't use turbines.
>>1216817
Diameter is the longest chord you can draw in a circle.and chord is a line between any two points on the circumference of the circle.
By waste heat you mean hot exhaust gases? They are made to pass though a de laval nozzle and out.
I know turbines have to be big to get TWR up, but I'm not pusing or flying anything with it. Just for graphs. And cars use turbine, it's called a turbocharger.
>>1216817
>dont do things for fun because it has no practical use!
fuck off
>>1216814
depends on what "high pressure" means to you. https://www.amazon.com/dp/B01N415WN5 is a $60 electric pump capable of 255 lph @ 43 psi and maxes at 120 psi. as for a tank im not sure how big a capacity you want but a something like a 1 gallon air tank (https://www.amazon.com/dp/B000YC7GAQ) would work well and obviously be able to handle 150+ psi.
also check out colin furze on youtube if you havent hes done a couple of turbo turbine projects, granted on propane, but still. even did one with no welding and it worked.
>>1216830
Will do. Thanks for the links anon.
>>1216814
>Wouldn't that cost a fortune to make/build?
Nah, the inject can be one like the ones you fund on diesel engines, but modify it so it releases a continuous flow. And the hydropneumatic is literally a pressurized can where you store a bit of fuel along with air at "high pressures" in order to ensure a steady flow, like a capacitor would work in a circuit