Mach Number Calculator (Speed & Temperature)

What this Mach number calculator does

Mach number (M) is a dimensionless way to express how fast an object is moving compared with the local speed of sound in the surrounding fluid. This calculator estimates Mach number in dry air from:

• Object speed (v) in meters per second (m/s)
• Ambient (outside) air temperature in °C

It also reports the speed of sound used in the calculation and classifies the result into common flight/flow regimes (subsonic, transonic, supersonic, hypersonic).

Key idea: Mach depends on temperature

Because the speed of sound changes with temperature, the same true airspeed can correspond to different Mach numbers on a cold day versus a warm day. In the lower atmosphere, temperature is the dominant factor; humidity and gas composition also matter but are not included in this simple model.

Formulas used

Mach number is defined as:

$$M=\frac{v}{a}$$

To estimate the speed of sound in dry air as a function of temperature in Celsius, this page uses the common near-surface linear approximation:

$$a=331.3+0.606T$$

where a is in m/s and T is in °C. (For more advanced work you’ll often see the ideal-gas form $a=\sqrt{\mathrm{\backslash gamma}RT}$ with temperature in Kelvin, but this calculator intentionally sticks to a simple, practical approximation.)

How to interpret your result

Mach number is frequently grouped into regimes that correspond to qualitatively different compressible-flow behavior:

• Subsonic (M < 0.8): compressibility effects are usually small.
• Transonic (0.8 ≤ M < 1.2): mixed subsonic/supersonic flow may occur; shocks can form and drag can rise rapidly.
• Supersonic (1.2 ≤ M < 5): sustained supersonic flow; shock waves and expansion fans dominate many design considerations.
• Hypersonic (M ≥ 5): high-temperature effects, strong shocks, and real-gas chemistry can become important.

Important: Mach number depends on the air-relative speed (airspeed) and the local temperature of the air the object is moving through. If you only know ground speed, wind can significantly change the air-relative speed and therefore Mach.

Worked example

Problem: An aircraft is traveling at 250 m/s in air at 15 °C. What is its Mach number?

1. Compute speed of sound:

   $$a=331.3+0.606\times 15$$

   That gives a ≈ 340.4 m/s.

2. Compute Mach number:

   $$M=\frac{250}{340.4}$$

   So M ≈ 0.735, which is subsonic.

Sensitivity & quick reference tables

1) Speed of sound vs. temperature (dry air approximation)

2) Typical Mach regimes and what they imply

Assumptions and limitations (read before using)

• Dry air approximation: Uses a = 331.3 + 0.606T. Humidity and CO₂ concentration can change a slightly.
• Temperature only: Does not model altitude directly. Altitude matters mainly because it changes temperature (and, in advanced models, gas properties).
• Local conditions: Uses the temperature you enter as the local ambient temperature where the object is moving. Atmospheric gradients, jet exhaust, or heating near surfaces are not considered.
• Not for real-gas/hypersonics design: At very high Mach numbers, dissociation, ionization, and non-ideal effects can make simple speed-of-sound estimates inaccurate.
• Input domain: If you enter very low temperatures, the linear model can predict non-physical values. The calculator will warn if the computed speed of sound is ≤ 0.

FAQ

What does Mach 1 mean?

Mach 1 means the object’s speed equals the local speed of sound in that air. Because the speed of sound changes with temperature, Mach 1 corresponds to different m/s at different temperatures.

Why does temperature affect Mach number so much?

In gases, the speed of sound scales with the square root of absolute temperature (and is well-approximated as nearly linear in °C over common weather ranges). Warmer air increases the speed of sound, so the same speed corresponds to a lower Mach number.

Should I use true airspeed or ground speed?

Use speed relative to the surrounding air (airspeed/true airspeed). Ground speed includes wind effects, which can change Mach significantly.