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Mach Number & Speed of Sound Calculator

The speed of sound in an ideal gas depends primarily on absolute thermodynamic temperature.

Speed of the aircraft or fluid in meters per second.

Ambient atmospheric temperature in degrees Celsius (standard sea level is 15°C).

Calculated Result
Mach 1.00

Flight Mach Number

Mach Number

Mach 1.00

Local Speed of Sound

340.3 m/s

Airspeed (km/h)

1,224.0 km/h

Flow Regime

Transonic (0.8 ≤ M ≤ 1.2)

Calculation Breakdown

  1. Local Speed of Sound in Ideal Gasa = √(1.4 × 287.058 × 288.15) = 340.30 m/s (1,225.1 km/h)a=γRspecificTa = \sqrt{\gamma R_{\text{specific}} T}
  2. Mach Number DefinitionM = 340.00 / 340.30 = Mach 0.999M=uaM = \frac{u}{a}
  3. Aerodynamic Flow RegimeTransonic (0.8 ≤ M ≤ 1.2)

Speed of Sound vs Air Temperature

Interactive visualization based on your current inputs

Speed (m/s)
0.088176264352-40°C-20°C0°C15°C35°CTemperature (°C)Sound Speed (m/s)

What Is the Mach Number & Speed of Sound Calculator?

The Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.

How Does the Mach Number & Speed of Sound Calculator Work?

Compressibility shock waves form when an object approaches or exceeds Mach 1, altering aerodynamic lift and drag.

Mach Number & Speed of Sound Calculator Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

a = \sqrt{\gamma R T}, \quad M = \frac{u}{a}

Speed of sound a depends on adiabatic index γ (1.4 for air), gas constant R (287 J/(kg·K)), and absolute temperature T. Mach number M is velocity divided by sound speed.

How to Use the Mach Number & Speed of Sound Calculator

  1. Enter true airspeed in meters per second.
  2. Specify air temperature in Celsius.

Step-by-Step Example Calculation

Standard Atmospheric Flight

Input Values:

speed:340
temperature:15
Worked Steps: At 15°C, sound travels at 340.3 m/s (1225 km/h). Moving at 340 m/s corresponds to Mach 0.999 (transonic threshold).

Understanding Your Result

Mach Number: Dimensionless flight speed ratio.

Local Sound Speed: True acoustic velocity at the specified ambient temperature.

Flow Regime: Categorized into Subsonic (<0.8), Transonic (0.8–1.2), Supersonic (1.2–5.0), or Hypersonic (≥5.0).

Factors That Affect the Result

  • Ambient Temperature: High altitude cold air (-56.5°C in the tropopause) drops sound speed to ~295 m/s (~1062 km/h).

When Should You Use This Calculator?

  • Aviation flight planning, compressible fluid dynamics, and supersonic wind tunnel analysis.

Assumptions & Limitations

  • Treats air as a dry, calorically perfect diatomic gas (γ = 1.4).

Frequently Asked Questions

Calculation Accuracy & Reference Note

Standard compressible gas dynamics formulation.

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