Mach Number Formula:
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The Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound. This specific formula calculates Mach number using wall temperature, static temperature, and specific heat ratio for large Mach numbers over a flat plate.
The calculator uses the Mach number formula:
Where:
Explanation: The formula relates the temperature ratio to the Mach number through the specific heat ratio, providing the flow velocity relative to the speed of sound.
Details: Mach number is crucial in aerodynamics and fluid dynamics for characterizing flow regimes (subsonic, transonic, supersonic, hypersonic) and analyzing compressibility effects in high-speed flows.
Tips: Enter wall temperature and static temperature in Kelvin, and specific heat ratio (must be greater than 1). All values must be valid positive numbers.
Q1: What is the significance of Mach number in fluid dynamics?
A: Mach number determines whether compressibility effects are important in a flow and classifies flow regimes from subsonic to hypersonic.
Q2: What are typical values for specific heat ratio?
A: For air at standard conditions, γ ≈ 1.4. For monatomic gases, γ ≈ 1.67, and for diatomic gases, γ ≈ 1.4.
Q3: When is this specific formula applicable?
A: This formula is particularly useful for calculating Mach number in high-speed flows over flat plates where temperature measurements are available.
Q4: What are the limitations of this calculation?
A: The formula assumes ideal gas behavior and may not be accurate for extremely high temperatures or pressures where real gas effects become significant.
Q5: How does wall temperature affect Mach number?
A: Higher wall temperature relative to static temperature generally results in higher Mach numbers, indicating faster flow velocities relative to the speed of sound.