The density (ρ) in the context of a CFM LEAP (Leading Edge Aviation Propulsion) engine or any gas turbine engine in aircraft design represents air density, which is the mass of air per unit volume. Air density varies with altitude, temperature, and pressure and can be calculated using the ideal gas law. The formula for air density (ρ) is:
– ρ is the air density (in kilograms per cubic meter, kg/m³).
– P is the atmospheric pressure (in pascals, Pa).
– R is the specific gas constant for dry air (approximately 287.05 J/(kg·K)).
– T is the absolute temperature (in kelvin, K).