I'm curious to know how AEFS calculates the critical Mach for swept back wings?
In such a wing, is the cosine of the full forward speed taken into consideration, or even a lower value due to the wings being finite, in order to proportionally reduce the effective Cl ? Like described i.e. in here: Why Do Fast Aircraft Have Swept Wings? | Boldmethod
And, if indeed this is taken into consideration where can I find references to the correction in the Wiki?