Plasma Channel Ion Thrust suggestions and ideas
Plasma Channel: Designing A Next-Gen Ionic Thruster! (For Flight) at https://www.youtube.com/watch?v=nrEBoPYS4ns The stagnation pressure is (1/2) * AirDensity*Velocity^2. And the power goes as the cube of the velocity. So using velocity increments is not exactly the best measure. At least get yourself a spreadsheet or HTML/Javascript and have it keep track of the velocity, squared velocity,
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