no way to compute mach number with FAR

[Assert1]

Mach number, is a key value of all aerodynamics processes, and everyting is linearized about it. It is required for any process modeling, but it can't be computed from the API with FAR installed.

[djungelorm]

Unfortunately this isn't exposed via FAR's public API :( I'll open a ticket with FAR and see if we can get it added.

[djungelorm]

Actually scratch that last comment, it is available, just via a vessel component instead of the FARAPI!