[bikalpa10]

Hi everyone,

I am trying to run optimization of delta wing Micro Air Vehicle having root chord 100mm and tip chord 1mm. My thickness are also decreasing similarly in a span-wise direction.
I want to give the upper and lower bound for optimization (movement limited to z-direction ) corresponding to 5% of the local chord. This value ranges from 5mm at the root to 0.05 mm tip.

Currently, SU2, takes a single variable as Upper or Lower bound input and applies the same for all cross-section/ design variable.

Is there any way to define, different upper and lower bound at different spanwise locations for shape optimization?

Thank you
regards
Bikalpa