The mass flow rate (ṁ) of dry Combustion in aircraft design is the mass of air passing through the compressor per unit of time. It can be calculated using the following formula:
– ṁ is the mass flow rate of air (in kilograms per second, kg/s).
– ρ is the density of the air (in kilograms per cubic meter, kg/m³).
– A is the cross-sectional area of the dry Combustion (in square meters, m²).
– V is the velocity of the air (in meters per second, m/s).