Turbojet engine thrust

[victorl21]

How can I calculate the thrust of my turbojet using the Brayton thermodynamic cycle data?

[racket]

You'll need to know your mass flow , the total temperature and pressure exiting the turbine wheel so that you can then calculate the potential velocity produced expanding the gases through the jet nozzle .

Then its a simple calculation , thrust = mass X velocity

Have a look at this postlmg.cc/phTQ3pGG also jetandturbineowners.proboards.com/thread/680/diy-turbines