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In aeronautics, the Mach number (named after the German physicist Ernst Mach) is the ratio of object speed to the speed of sound. At sea level (and at 20°C), sound travels 340 m/s, or about 1,224 km/h; the speed of sound declines slightly with altitude, and at 11 kilometers above sea level, a typical cruising altitude for jetliners, it is about 295 m/s or 1,063 km/h, and hence a Boeing 787 cruising at 903 km/h will fly at M 0.85. All speeds of M < 1 are subsonic; transonic is the term used for speed in the vicinity of M, and the supersonic range is 1 < M < 3.
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