The mass flow rate of air in a combustion chamber is a crucial parameter that represents the rate at which air is entering the combustion chamber. It’s essential for combustion analysis and aircraft design.
The formula to calculate the mass flow rate of air can be defined as follows:
- Mass Flow Rate of Air is the rate at which air is entering the combustion chamber, typically measured in kilograms per second (kg/s) or pounds per second (lb/s).
- Air Density represents the density of the incoming air, typically measured in kilograms per cubic meter (kg/m³) or slugs per cubic foot (sl/ft³).Inlet Velocity is the velocity or speed of the incoming air, typically measured in meters per second (m/s) or feet per second (ft/s).
- Cross-Sectional Area is the area of the inlet or entry point through which air is flowing, typically measured in square meters (m²) or square feet (ft²).