Hello!
I am back and we are now trying to implement stability derivatives using the SCT to find the different terms with respect to u, alpha, q, and alpha dot. My question mostly lies with the alpha dot terms, as there is no way to set the denominator of the derivatives to be alpha dot (essentially downwash and the associated lag with the tail). I thought to maybe use an unsteady solver but that did not add any additional options.
I would like to take these stability derivatives and do my own dynamic stability analysis and modal analysis but I am just having trouble getting the correct things I will need.
Thanks!