Ideal Gas HW Problem: Pressure at 11,000 meters?

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SUMMARY

The problem involves calculating atmospheric pressure at an altitude of 11,000 meters with a temperature of -50 degrees Celsius and an air density of 0.403 kg/m^3. The equation used was P = P0exp(-Mgy/RT), but the solution of P = 2.8 * 10^4 was not accepted by the online homework system. The correct approach is to utilize the Ideal Gas Law for accurate results, specifically considering the standard atmospheric pressure at sea level and the temperature conversion to Kelvin.

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  • Basic principles of gas density and altitude effects
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Ideal Gas HW Problem!?

Homework Statement


"At an altitude of 11,000 meters, the air temperature is -50 degrees celsius. The air density is 0.403 kg/m^3. What is the pressure of the atmosphere at that altitude."

Homework Equations


P = P0exp(- Mgy/RT)


The Attempt at a Solution


I attempted to solve the problem using the above equation above equation and my result was P = 2.8 * 10^4. However my online homework is not accepting the answer and I'm not sure what I did wrong. Any help would be greatly appreciated!
 
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Po is the pressure at altitude h=0, at the given temperature. I think you used the value given for T=273 K.

Use the Ideal Gas Law instead.

ehild
 

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