Find mach number of plane for the stated limiting conditions


The Airbus A-340 plane has a maximum takeoff weight of about 260,000kg, a length of 64m, a wing span of 60m, a maximum cruising speed of 945km/h, a seating capacity of 271 passengers, maximum cruising altitude of 14, 000 m, and a maximum range of 12, 000km. The air temperature at the cruising altitude is about -60 degrees celcius. Determine the Mach number of this plane for the stated limiting conditions.

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Mechanical Engineering: Find mach number of plane for the stated limiting conditions
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