The formula for calculating the throat area of a nozzle depends on the shape of the nozzle. In the case of a converging-diverging (CD) nozzle, which is commonly used in aerospace engineering.
Where:
- is the throat area,
- is the diameter of the throat.
The formula for calculating the throat area of a nozzle depends on the shape of the nozzle. In the case of a converging-diverging (CD) nozzle, which is commonly used in aerospace engineering.
Where: