Mach Number Equation:
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The Mach number (M) is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound. It's a critical parameter in aerodynamics and fluid dynamics, especially for high-speed flows.
The calculator uses the following equations:
Where:
Explanation: The calculator first determines the temperature at the given altitude using the standard atmosphere lapse rate, then calculates the Mach number based on the speed of sound at that temperature.
Details: Mach number is crucial in aerodynamics for determining compressibility effects. Different flow regimes (subsonic, transonic, supersonic, hypersonic) are defined by Mach number ranges.
Tips: Enter velocity in m/s, altitude in meters, and specific heat ratio (1.4 for air). All values must be valid (velocity > 0, altitude ≥ 0, γ between 1-2).
Q1: What is the speed of sound at sea level?
A: Approximately 343 m/s (761 mph) at 20°C (293 K), but it varies with temperature.
Q2: What are typical Mach number ranges?
A: Subsonic (M < 0.8), Transonic (0.8 < M < 1.2), Supersonic (1.2 < M < 5), Hypersonic (M > 5).
Q3: Why does temperature decrease with altitude?
A: In the troposphere (up to ~11 km), temperature decreases with altitude due to decreasing pressure and adiabatic expansion.
Q4: What's the difference between true Mach and calibrated Mach?
A: True Mach uses actual speed of sound, while calibrated Mach corrects for instrument errors at high speeds.
Q5: How accurate is this calculator?
A: It uses standard atmospheric model which is accurate for general purposes but doesn't account for weather variations.