Atmospheric Density - Equation to Model from Sea Level to 200km

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    Atmospheric Density
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SUMMARY

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.

PREREQUISITES
  • Understanding of the ideal gas law and its application in atmospheric science
  • Familiarity with exponential functions and their use in modeling
  • Basic knowledge of atmospheric pressure and density concepts
  • Proficiency in using Excel for data analysis and graphing
NEXT STEPS
  • Research the Barometric formula for atmospheric pressure calculations
  • Explore the Standard Atmosphere models, specifically US and ICAO variations
  • Learn about the impact of solar activity on atmospheric density
  • Investigate fluid mechanics texts for comprehensive tables and formulas related to atmospheric modeling
USEFUL FOR

Atmospheric scientists, aerospace engineers, and students studying fluid mechanics or environmental science will benefit from this discussion on atmospheric density modeling.

ZachWeiner
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Hey, does anyone have an equation that roughly models atmospheric density from sea level to about 200 km up?
 
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There's not much of an equation for atmospheric pressure that's simple. If you have a CRC handbook you could look up a few values. You should know, as well, that it's quit variable at higher altitudes, dependent on solar activity.
 
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.
 
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.

I have no excuse for it, but in response to this question, I actually tried an exponential curve of pressure vs. height, and fit it to two points of data; sea level and 100 Km. It was off by 28% at 50 Km. Very disappointing.

To get a decent curve fit, P = P0 * exp(ah^3 + bh^2 + h) might do it.
 
what do you need to model it for? pretty much any fluid mechanics text will tell you in a table at the back.

lol.. if u really want to model it, put all the numbers into excel and graph it
 
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