How can air density be accurately calculated at different altitudes?

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SUMMARY

The accurate calculation of air density at various altitudes, specifically at 15 km and 7.5 km, can be derived using the formula D1/D2 = 4*p1/p2, where p represents air density at respective heights. Given air densities of 0.38 kg/m³ at 10 km and 0.67 kg/m³ at 5 km, the correct air density at 15 km is determined to be 3.3 kg/m³. The discussion emphasizes the inadequacy of linear estimations for air density calculations, advocating for a more complex modeling approach, such as exponential functions, despite the challenges in applying them to fundamental physics.

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  • Understanding of atmospheric physics and density calculations
  • Familiarity with exponential functions and their applications
  • Basic knowledge of logarithmic functions and graphing
  • Experience with density measurements at varying altitudes
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  • Research the application of exponential models in atmospheric science
  • Study the relationship between altitude and air density using logarithmic graphs
  • Explore advanced atmospheric density calculation methods
  • Investigate the impact of temperature variations on air density
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Addez123
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Homework Statement
A plane flies at a height of 15km with velocity of 1200km/h.
Another plane flies at half that speed and altitude.

Air density at 10km is .38
Air density at 5km is .67

Assume they have same cross section area A and drag coefficient C.
Calculate the ratio of the dragforce of the two planes.
Relevant Equations
D = 1/2 * CpA*v^2
Just calculating D1 (15km altitude plane) and D2 (7.5km altitude plane) turns out to;
D1/D2 = 4*p1/p2
p being the air density at each height.

How am I suppose to calculate p? We have had no such formulas, not to mention it depends on temprature etc.
Doing a linear estimation will yield wrong answer.

Correct answer is 3.3
 
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Addez123 said:
How am I suppose to calculate p?
You are given ##\rho##.
The problem statement said:
Air density at 10km is .38
Air density at 5km is .67
 
I'm given air density for 10 and 5km. I need air density for 15 and 7.5km.
 
Addez123 said:
I'm given air density for 10 and 5km. I need air density for 15 and 7.5km.
Ahah. That makes more sense.

Suppose that you model the atmospheric density as an exponential function of altitude. If a 5 km delta in height results in a factor of ##\frac{0.38}{0.67}## reduction in density, What ratio would one expect for a 7.5 km delta?
 
I seriously doubt we're ment to estimate an exponential function. That's more of a math question, this is suppose to be fundamental physics. Appriciate the suggestion tho!
 
Addez123 said:
I seriously doubt we're ment to estimate an exponential function. That's more of a math question, this is suppose to be fundamental physics. Appriciate the suggestion tho!
You've never been set a problem with radioactive half-lives?
 
Make a graph of log-density vs altitude. Don’t forget to include density 1 at z = 0. It should be virtually a straight line.
 
Chestermiller said:
Make a graph of log-density vs altitude. Don’t forget to include density 1 at z = 0. It should be virtually a straight line.
Interesting. For these figures, it is not even close to a straight line.
 
jbriggs444 said:
Interesting. For these figures, it is not even close to a straight line.
You're right. For this data, a liner fit seems to work best. Of course, that's now how the real atmosphere works.
 

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