ZachWeiner
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Hey, does anyone have an equation that roughly models atmospheric density from sea level to about 200 km up?
The discussion centers on modeling atmospheric density from sea level to 200 km using specific equations. The primary formula presented is P = (Patm) * e^(-Mgh/RT), where Patm represents sea level pressure, and D = PM/RT for density calculation. It is noted that this model assumes constant temperature, making it suitable only for rough estimates. Alternative approaches, including exponential curve fitting and referencing standard atmospheres, are also discussed for more accurate modeling.
PREREQUISITESAtmospheric scientists, aerospace engineers, and students studying fluid mechanics or environmental science will benefit from this discussion on atmospheric density modeling.
aniketp said:Hi ZachWeiner,
Pressure at a height "h" is given by :
P=(Patm)*e^(-Mgh/RT) [Patm is the pressure at sea level]
And D=PM/RT
But there is an assumption that T is const. this formula will only enable you to calculate the density roughly. So do not use it if you want accurate answers.