I am so sorry to bother you with another issue I am facing. I have set up a new configuration in SUAVE for analyses and I am running into an error where the lift coefficient generated is very small in the order of 0.03 and the Propeller coefficient graph provides a 0 thrust plot and negative tip Mach, and Cp. I am not sure where I can go to solve the error. I have already tried to change the motor, prop and battery size to get better results but haven't got any better results.
Here is the plot as I am getting it currently
Where can I find the iterative loop that calculates the thrust for every iteration and what does that loop call and pass trough? Is the thrust being calculated for each time step?
I am not sure what I need to look at to solve this, as the code is very sensitive as far as I have seen and thus a few changes affects a lot of things in the code.
Hope to hear from you soon.