Sonic Flow Formula:
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Definition: This calculator determines the mass flow rate of gas through a nozzle when the flow is choked (sonic conditions at the throat).
Purpose: Used in engineering applications to measure or predict gas flow rates in pipelines, ventilation systems, and process equipment.
The calculator uses the isentropic flow equation for choked conditions:
Where:
Explanation: The equation accounts for gas properties and choked flow conditions where velocity at the throat equals sonic velocity.
Details: Accurate flow measurement is critical for system design, safety, and efficiency in gas handling systems.
Tips: Enter the discharge coefficient (default 0.98), nozzle area, upstream pressure, specific heat ratio (default 1.4 for air), gas constant (default 53.3 for air), and absolute temperature in Rankine.
Q1: When does flow become choked in a nozzle?
A: Flow becomes choked (sonic at throat) when downstream pressure is ≤ ~53% of upstream pressure for air (γ=1.4).
Q2: What's a typical discharge coefficient?
A: Well-designed nozzles typically have Cd between 0.95 and 0.99.
Q3: How do I convert temperature to Rankine?
A: °R = °F + 459.67. The calculator requires absolute temperature.
Q4: What's the gas constant for common gases?
A: Air = 53.3, Nitrogen = 55.2, Oxygen = 48.3, Hydrogen = 766.5 ft·lb/lb·°R.
Q5: Can I use this for subsonic flow?
A: No, this equation is only valid for choked (sonic) flow conditions.