Mach Number Calculator
Mach Number: a planned Super Calculator tool. Covers true airspeed and static air temperature. Stub page while the tool and its worked example are prepared.
Mach Number Calculator is a planned calculator in the transport section of Super Calculator, covering air data.
What this calculator will compute
Inputs: true airspeed and static air temperature.
Formula, recorded as scope and not yet verified against a primary source: M = TAS divided by speed of sound, a = 38.967854 times sqrt(T in kelvin).
Written for turbine pilots and aviation students crossing the mach transition altitude.
Status
This page is a stub. The calculator is not built, no figure on this page has been verified against the authority that sets it, and nothing here should be used to make a decision. The page exists so that the site structure is complete and so that articles can link this concept on first mention.
The stub carries noindex, nofollow and is excluded from the sitemap.