In aircraft design, the density of a fluid passing through a convergence nozzle can be calculated using the ideal gas law. The formula for density is as follows:
- ρ = Density of the fluid (in kilograms per cubic meter, kg/m³)
- P = Pressure of the fluid (in pascals, Pa)
- R = Specific gas constant for the fluid (in J/(kg·K))
- T = Temperature of the fluid (in kelvin, K)