In flight mechanics and aerodynamics, the “Mach number” (often denoted as ) is a dimensionless parameter that represents the ratio of an aircraft’s velocity to the local speed of sound in the surrounding air. It is a crucial parameter used to describe an aircraft’s speed relative to the speed of sound and is used to categorize the aircraft’s flight regime.
Where:
- is the Mach number.
- is the velocity of the aircraft.
- is the local speed of sound in the air.