Mach Number Calculator

Convert between true airspeed and Mach number at any air temperature

Convert between true airspeed and Mach number using the standard speed-of-sound formula a equals the square root of gamma R T. Enter static air temperature and TAS or Mach to get the other, plus the local speed of sound, for cruise speed management. It runs free in your browser on Gera Tools, with nothing uploaded.

Last updated Source: Gera Tools

How is Mach number calculated?

Mach number is true airspeed divided by the local speed of sound. The speed of sound is the square root of gamma times R times T, where gamma is 1.4 for air, R is 287 joules per kilogram kelvin, and T is the static air temperature in kelvin.

High and fast, pilots manage speed by Mach number rather than airspeed, because the limits that matter — buffet, shock-induced drag, and Mmo — are tied to the speed of sound, not the airspeed indicator. This calculator converts between true airspeed and Mach number at any temperature and shows the local speed of sound.

How it works

Mach number is true airspeed divided by the local speed of sound. The speed of sound a follows the standard relation a = sqrt(gamma x R x T), which for dry air simplifies to a = 20.0468 x sqrt(T) metres per second, with T the static air temperature in kelvin. Crucially the speed of sound depends only on temperature — not pressure or altitude directly.

The tool converts your temperature to kelvin, computes the speed of sound in knots and metres per second, then divides TAS by it to get Mach, or multiplies Mach by it to get TAS.

Worked example

At minus 50 degrees Celsius the speed of sound is about 575 kt. A true airspeed of 450 kt is therefore about Mach 0.78. The same 450 kt down at plus 15 degrees Celsius, where the speed of sound is about 661 kt, is only Mach 0.68 — the same airspeed, a very different Mach number.

Notes

The dry-air formula ignores humidity and pressure, which is accurate to a fraction of a percent for flight. Always respect the published Mmo and the barber-pole on the airspeed indicator; this tool is for speed management, not for exceeding limits.

Why Mach number is used at cruise altitude

At sea level, pilots fly by indicated airspeed (IAS), which is what the pitot-static system measures directly. Below roughly 25,000–30,000 ft, structural limits are airspeed-based — the aircraft’s skin and control surfaces can only tolerate so much dynamic pressure regardless of altitude.

Above the tropopause (roughly FL360 in standard atmosphere), air temperature stabilizes near −56.5 °C, so the speed of sound is nearly constant. In this regime, the limits that matter — critical Mach number (onset of transonic drag rise), MMO (maximum operating Mach), and buffet onset — are all fractions of the speed of sound. It makes more sense to fly at a fixed Mach than at a fixed airspeed that would require continuous adjustment as altitude and air density change.

Standard atmosphere temperature profile

Temperature in the standard atmosphere decreases with altitude at the International Standard Atmosphere (ISA) lapse rate of −6.5 °C per 1,000 ft until the tropopause:

Pressure altitudeISA temperatureSpeed of sound (approx)
Sea level+15 °C661 kt
FL100−5 °C638 kt
FL200−25 °C614 kt
FL360+ (tropopause)−56.5 °C575 kt

Enter the actual static air temperature (SAT) from your flight management system or weather charts rather than assuming ISA — deviations from standard can meaningfully shift the Mach number for a given TAS.

Mmo versus critical Mach number

These are distinct limits that are often confused:

  • Critical Mach number (Mcrit) is the TAS at which airflow over the thickest part of the wing first reaches Mach 1 locally, creating a shock wave. This is an aerodynamic threshold set by wing geometry.
  • Mmo is the certificated maximum operating Mach number, a regulatory structural and handling-qualities limit below which the aircraft must remain. It appears as a barber-pole on the airspeed indicator and is typically set several Mach below Mcrit with a comfortable margin.

Exceeding Mmo does not cause immediate structural failure, but it risks Mach tuck (pitch-down tendency from shock-wave migration), reduced control effectiveness, and potential structural overload — all good reasons to stay comfortably below the barber-pole.

Practical use: crossover altitude

Pilots switching from airspeed to Mach at the crossover altitude need to know the TAS at which the two limits intersect. Below the crossover, the airspeed limit is binding; above it, the Mach limit is. This tool lets you verify the TAS that corresponds to your cruise Mach at the actual temperature for your flight level, which is useful for cross-checking the FMS or briefing non-type-rated observers.