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bjhello
14th Feb 2006, 08:13
Hey guys

Is there a way to calculate mach out of IAS, TAT and ALT?

Not rule of dump.

Maybe a formula?

Thnks for the help :ok:

BJ

leftright
14th Feb 2006, 09:58
yes there is...

Mach= TAS/(38.94*SQR(273+SAT))

Alex Whittingham
15th Feb 2006, 07:36
Aviation Formulae (http://williams.best.vwh.net/avform.html)