xnor

But it allows asymmetric foils which at least allows rudimentary simulations with different aileron and flap positions, and it also seems to calculate the torque ("L"?) around the longitudinal axis. How else could I simulate something like tailerons? Or do you know of any simple way to calculate the torque based on air stream velocity, wing/control surface area/dimensions and angle of attack? Are there any rules of thumb how to dimension these to get a desired roll rate?

Hello, I would like to simulate a flying tailplane where the left and right side have different angles. How do I do this? Also, I would like to simulate the effects of asymmetric dihedral and twist of the wing. Is that possible?

So does this bug need to be reported somewhere else?

Years later, 64 bit binaries produced with -flto still crash. Is there ever going to be a fix for this?

I know that the daemon will overwrite settings. Changes might have indeed been lost...

One restart later and peer-limit-global was again reset to 0. Do I have to make settings.json...

One restart later and peer-limit-global was again reset to 0. Do I have to make settings.json...

I found out what caused the "http error 0" error: "bind-address-ipv6" was set to...