Sure, I would be happy to help you find the air density formula you are looking for. The relationship between air temperature and pressure-altitude is described by the ideal gas law, which states that the density of a gas is directly proportional to its temperature and inversely proportional to its pressure. This can be expressed mathematically as:
ρ = (P / RT)
Where ρ is the air density, P is the pressure, R is the gas constant, and T is the temperature in Kelvin.
To incorporate pressure-altitude into this formula, you will need to convert the pressure into its corresponding altitude. This can be done using the International Standard Atmosphere (ISA) model, which assumes a standard lapse rate for temperature and pressure changes with altitude.
The formula for converting pressure into altitude using the ISA model is:
h = [1 - (P / P0)^0.190284] * 145366.45
Where h is the altitude in feet, P is the pressure in pounds per square inch (psi), and P0 is the pressure at sea level, which is 14.696 psi.
Combining these formulas, we can find the air density at a specific altitude and temperature using the following equation:
ρ = (P / RT) * [1 - (P / P0)^0.190284] * 145366.45
I hope this helps you find the air density formula you were looking for. Let me know if you have any further questions or need clarification on anything. Best of luck!