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I'm looking for a formula that will find the air density based on a relationship between air temperature and pressure-altitude. Any help would be greately appreciated!
The air density can be calculated using the ideal gas law, expressed as ρ = (P / RT), where ρ is air density, P is pressure, R is the gas constant, and T is temperature in Kelvin. To incorporate pressure-altitude, the International Standard Atmosphere (ISA) model is utilized, converting pressure to altitude with the formula h = [1 - (P / P0)^0.190284] * 145366.45, where P0 is the sea level pressure of 14.696 psi. The combined formula for air density at a specific altitude and temperature is ρ = (P / RT) * [1 - (P / P0)^0.190284] * 145366.45.
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