I understand how to find trim conditions and a stability analysis for level flight where L=W. However, if I want to conduct a trim analysis for climb or descent where L=Wcos(gamma), trimmed by elevator deflection, how would I proceed to give these flight conditions to XFLR5 for a stability analysis?
If you would like to refer to this comment somewhere else in this project, copy and paste the following link:
Hello,
I understand how to find trim conditions and a stability analysis for level flight where L=W. However, if I want to conduct a trim analysis for climb or descent where L=Wcos(gamma), trimmed by elevator deflection, how would I proceed to give these flight conditions to XFLR5 for a stability analysis?