The mass flow rate through a convergence nozzle in aircraft design can be calculated using the principles of fluid dynamics. The formula for mass flow rate m is as follows:
- m is the mass flow rate (in kilograms per second, kg/s).
- A is the cross-sectional area of the nozzle (in square meters, m²).
- rho is the density of the fluid (in kilograms per cubic meter, kg/m³).
- V is the velocity of the fluid (in meters per second, m/s).