[aero_amit]

Dear Developers,

What is the procedure for mesh adaptation in SU2-V4.

After obtaining the steady state solution for NACA airfoil at transonic Mach number, I tried mesh adaptation by running SU2_MSH configfile.cfg.

In .cfg file I am setting option as -

KIND_ADAPT= GRAD_FLOW
or
KIND_ADAPT= SUPERSONIC_SHOCK

This is not adapting to the shock and randomly adapting to other places.

Is there any step i am missing (copying solution file to appropriate name etc.) ?

Kindly help in figuring out the correct procedure (steps).

Thanks and Regards
Amit