Dear Altair Team,
how exactly does the "No. comp. / elec. period" influence the over all simulation time when including rotor position dependency. Regarding a previous question ("How much does the rotor position dependency increase the simulation time"), where I simulated an EESM, I would like to know how the "No. comp. / elec. period" influences simulations and when is using 1/2 period and when 1 period is recommended.
Thank you in advance.