Mach Number Calculator

Mach number is the ratio of object speed to the local speed of sound. M<1 is subsonic, M=1 is sonic, M>1 supersonic, M>5 hypersonic. It changes with altitude since sound speed varies with temperature.

💨 Fluid Dynamics📐 M = v/vₛ✈️ Aerodynamics
Object Speed v (m/s)
Speed of Sound vs (m/s)

Default sound speed 343 m/s (sea level 20°C)

Please enter valid values.

Formula & Reference

VariableSymbolFormulaUnits
Mach NumberMM = v / vsdimensionless
Object Speedvv = M × vsm/s
Speed of Soundvs331.3√(T/273.15)m/s
At sea level 20°Cvs343 m/sm/s

Step-by-Step Examples

Example 1
Commercial Jet

Boeing 747 at 900 km/h, vs=295 m/s at cruise altitude.

  • v = 900/3.6 = 250 m/s
  • M = 250/295 = 0.847
✓ Mach 0.847 — high subsonic
Example 2
Concorde

Mach 2.04 target, vs=295 m/s.

  • v = 2.04 * 295 = 601.8 m/s = 2166 km/h
✓ 2166 km/h supersonic
Example 3
Rifle Bullet

v = 900 m/s, vs = 343 m/s.

  • M = 900/343 = 2.62
✓ Mach 2.62 — supersonic bullet

Real-World Applications

✈️
Aircraft Design
Wings designed for specific Mach regime — subsonic and supersonic require very different shapes.
🚀
Rocket Nozzles
Nozzle throat reaches Mach 1, supersonic flow in diverging section via de Laval geometry.
💥
Sonic Boom
Shock wave forms when M=1 is crossed. Boom heard when cone passes observer.
🌡️
Altitude Effect
Sound speed drops with altitude — Mach 1 at 10 km is 299 m/s vs 343 m/s at sea level.

Common Mistakes to Avoid

⚠️
Speed of sound varies with altitude

At 10,000 m altitude, vs ~299 m/s due to colder air. Always use correct vs for altitude.

⚠️
Mach 1 is not a fixed speed

Mach 1 = local sound speed. An aircraft at Mach 1 flies slower at sea level than the statement implies.

⚠️
Transonic regime is complex

Between M=0.8 and 1.2, mixed subsonic/supersonic flow creates complex shock patterns requiring special aerodynamic design.

Frequently Asked Questions

What happens exactly at Mach 1?
A normal shock wave forms at the nose. Pressure, density, and temperature jump discontinuously across it. This creates the sonic boom.
Why do jets not cruise at Mach 1?
Wave drag peaks near M=1 (transonic drag rise). Requires too much fuel. Commercial jets cruise at M=0.83-0.89 to avoid this.
What is hypersonic flight?
M > 5. Aerodynamic heating becomes extreme (SR-71 skin reached 300 deg C). Chemical reactions in air must be considered.
How does a Mach cone form?
At supersonic speed, object outruns sound waves. Cone half-angle theta satisfies sin(theta) = 1/M.
What was the first supersonic aircraft?
Chuck Yeager in the Bell X-1 broke Mach 1 on October 14, 1947, reaching Mach 1.06 at 13,000 m altitude.

Related Physics Calculators

Formula Explorer connections

Interpretation: This relationship connects pressure, velocity, density, viscosity, geometry or transport in a fluid system. Assumption: Check whether flow is steady, incompressible, laminar, fully developed or one-dimensional. Reynolds and Mach regimes determine whether simplified formulas are valid.

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