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Question

Calculate the pressure of a barometer on an aeroplane which is at an altitude of 10 Km. Assume the pressure to be 101.325 Kpa at sea level and the mean temperature 243 K. Use the average molar mass of air (80% N2,20% O2).

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Solution

M=0.8×0.028+0.2×0.032=0.0288
ln101.325p=0.0288×9.8×100008.3×243
p=25.027kpa

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