The cross-sectional area of a divergence nozzle in aircraft design can be calculated using the following formula:
- A is the cross-sectional area through which Divergence Nozzle (in square meters, m²).
- ṁ is the mass flow rate in kilograms per second (kg/s).
- ρ is the air density in kilograms per cubic meter (kg/m³).
- V is the velocity of the Divergence Nozzle (in meters per second, m/s).