Mach Number Calculator
Compare object speed to local sound speed (subsonic / sonic / supersonic)
Parameters
Controls
Calculated Values
Examples
Supersonic jet
v = 686 m/s, v_s = 343 m/s.
Subsonic aircraft
v = 250 m/s.
Visualization
Mach Number — Comparing Speed to Sound Speed
The Mach number Ma = v/v_s is a dimensionless ratio of the speed of an object (or flow) v to the local speed of sound v_s in the surrounding medium. It tells whether disturbances (sound waves) can outrun the object.
Subsonic (Ma < 1): the object moves slower than sound. Pressure disturbances propagate ahead, warning the medium. Air flows smoothly in many cases; wings and cars often operate subsonically.
Sonic (Ma = 1): object speed equals sound speed. Drag rises sharply in the transonic regime (Ma ≈ 0.8–1.2) due to shock formation and wave drag. “Breaking the sound barrier” means crossing Ma = 1.
Supersonic (Ma > 1): the object outruns its sound waves. A Mach cone forms; shock waves produce sudden pressure jumps. A sonic boom is heard when shock waves from a supersonic aircraft reach the ground.
Sound speed in an ideal gas: v_s = √(γRT/M), where γ ≈ 1.4 for air, R is gas constant, T is absolute temperature (K), M is molar mass. At 20°C (293 K), v_s ≈ 343 m/s in dry air. Hotter air → faster sound → higher v_s.
Example: jet at v = 686 m/s in air with v_s = 343 m/s → Ma = 2 (supersonic). Concorde cruised at Ma ≈ 2. Fighter aircraft exceed Ma 2; spacecraft re-entry reaches Ma > 20 in the atmosphere.
Mach number differs from Doppler effect: Doppler shifts observed frequency when source and observer move relative to each other; Mach number compares source speed to v_s in the medium. Class 12 Doppler; engineering uses Ma for aerodynamics.
Key Concepts
- Ma = v/v_s
- Subsonic Ma < 1
- Sonic Ma = 1
- Supersonic Ma > 1
- v_s ≈ 343 m/s at 20°C in air
- v_s = √(γRT/M) ideal gas
Real-World Applications
- Aircraft, missile, and spacecraft aerodynamics
- Wind tunnel and CFD Mach scaling
- Sonic boom and supersonic transport
- Astrophysical shocks (supernova, bow shocks)
- Class 12–JEE Mach and Doppler concepts
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Physics Equations
Step-by-Step Solution
See how the main results are calculated.
Step 1: Mach Number
Equation:
Explanation:
Ratio of object speed to local sound speed.
Step 2: Given
Result:
Step 3: Calculate
Calculation:
Result:
Step 4: Regime
Supersonic — shock waves form
Explanation:
At Ma = 1, sound and object move together.
Step 5: Doppler Connection
High Ma implies strong compression (bow shock) and sonic boom when Ma crosses 1.
Explanation:
Sound speed depends on medium temperature.
Step 6: Typical vₛ
Air at 20°C: vₛ ≈ 343 m/s
Explanation:
vₛ = √(γRT/M) for ideal gas.
Frequently Asked Questions (FAQ)
What causes a sonic boom?
Shock waves from supersonic flight merge into a N-wave pressure pulse heard on the ground when the aircraft is at suitable altitude and speed.
Mach number in water?
Use v_s ≈ 1500 m/s. A torpedo at 30 m/s has Ma ≈ 0.02 — still subsonic in water.
Is Ma the same as speed?
No. Ma depends on both v and local v_s (temperature, medium). Same v gives different Ma in hot vs cold air.
Hypersonic?
Often Ma > 5. Extreme heating and dissociation of air; re-entry vehicles face this regime.
Relation to Doppler?
Doppler: observer hears shifted f when source moves. Mach: ratio v/v_s in medium; sonic boom is shock physics, not simple Doppler.
Practice MCQs
- Mach number:
- Ma = 2 means:
- v_s in air ~
- Sonic flight Ma:
- Shock waves when:
- Higher temperature air:
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