(adsbygoogle = window.adsbygoogle || []).push({}); 1. The problem statement, all variables and given/known data

Calculate the pressure and density of nitrogen at which there is a 15% error in the ideal gas equation of state for a plane flying in air of temperature 250 K

2. Relevant equations

P = rho RT

Pv = RT

3. The attempt at a solution

Little confused on how to approach the problem. Any guidance is appreciated.

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# Guidance on finding the pressure and density of nitrogen

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