The velocity (V) of dry Combustion in aircraft design refers to the speed at which air flows through the compressor. It can be calculated using the following formula:
– V is the velocity of air (in meters per second, m/s).
– 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).