High Speed Flow Fluid Mechanics Dimensionless Value
Solve for Weber number.
Subsonic: | M<1 |
Transonic: | M=1 |
Supersonic: | M>1 |
Hypersonic: | M>5 |
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![]() | Mach number |
![]() | object speed |
![]() | speed of sound |
The Mach number is a key concept in fluid dynamics. It represents the object's speed to the sound speed in the surrounding medium ratio. Named after physicist Ernst Mach, this dimensionless number is crucial when analyzing compressible flows, especially in high-speed scenarios like aerospace, defense systems, and atmospheric science.
Understanding the Mach number helps determine how gases behave around moving objects. At lower speeds, air behaves predictably, but at higher speeds—especially near or beyond the speed of sound—compressibility effects become significant. These effects can cause shock waves and changes in pressure and temperature, which are essential to consider in design and analysis.
The Mach number (M) is defined as:
M = v / a
Where:
The speed of sound depends on the temperature and properties of the medium. In dry air at sea level and 20°C, the sound speed is approximately 340 m/s.
Determine the object's velocity (v): Use instrumentation or known values to determine the object's speed.
Determine the speed of sound (a): Use tables, equations, or environmental data for the medium's sound speed.
Divide velocity by the speed of sound: M = v / a
Problem: An aircraft travels at 600 m/s at an altitude where the speed of sound is 295 m/s. What is its Mach number?
Solution:
M = 600 / 295 = 2.03
This means the aircraft is traveling at Mach 2.03, which is considered supersonic.
Lindeburg, Michael R. 1992. Engineer In Training Reference Manual. Professional Publication, Inc. 8th Edition.
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