The ratio of flow velocity to the local speed of sound, indicating compressibility effects.The Mach number is a dimensionless quantity in fluid dynamics that compares the speed of an object or flow to the local speed of sound in the surrounding medium. It is a critical parameter for understanding compressibility effects: at low Mach numbers (below ~0.3), air can be treated as incompressible, while at higher values, density changes become significant, leading to shock waves, sonic booms, and dramatic changes in drag and lift. The Mach number is not just a number; it defines entire regimes of flight—subsonic, transonic, supersonic, and hypersonic—each with its own physical phenomena.
The concept was introduced by Austrian physicist Ernst Mach in the late 19th century. He studied projectile motion and used schlieren photography to visualize shock waves, naming the ratio in his honor. The term 'Mach number' was coined later, in 1929, by the Swiss engineer Jakob Ackeret.
The speed of sound in a medium depends on its temperature and composition. The Mach number is calculated as M = v/a, where v is the flow velocity and a is the local speed of sound. When M < 1, disturbances (like sound waves) propagate faster than the object, so the flow 'warns' the air ahead. When M > 1, the object outruns its own pressure waves, causing them to pile up into a shock front—a thin region where pressure, temperature, and density jump abruptly. This shock wave is what creates the sonic boom and the characteristic 'wall' of high drag at transonic speeds.
The Mach number is essential for designing aircraft, rockets, and wind tunnels. It is used to predict shock wave formation, optimize airfoil shapes for supersonic flight, and ensure the structural integrity of vehicles crossing the sound barrier.
In the exotic world of quantum fluids, the concept of a 'Mach number' applies to superfluid helium-3, where the 'sound' is replaced by collective excitations, and exceeding the critical velocity creates quantum vortices instead of shock waves.
| \mathcal{M} | variable | Mach number — mach number |
| v | variable | flow velocity — velocity metre per second |
| c_s | variable | local speed of sound — speed of sound metre per second |



