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Post by davidhaaland on Jan 23, 2024 4:28:31 GMT -5
Are there any equations or specifications for designing the nozzle for the DIY gas turbine engine? I.e., the right dimensions. I heard that lowering the nozzle exit area increases thrust and that you want a kind of an ellipse. Additionally, how to design the lubrication system.
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Post by racket on Jan 23, 2024 14:54:00 GMT -5
The nozzle area needs to be small enough to provide the correct backpressure on the engine so that running temperatures are within safe limits , too small a nozzle and you'll over temp the engine and damage the turbine wheel . Read these jetandturbineowners.proboards.com/thread/680/diy-turbines click on the icons for the info |
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