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Density (kg/m) Enthalpy (kJ) Thermal conductivity (W/m-K) Specific heat capacity (kJ/kg K) Mass (kg) Problem 4 A barometer at
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Answer #1

Problem 4

Given : P1 = 101 kPa

P2 = 85 kPa

air density = 1.2 kg/m3

Formula used : \small \Delta P = (\small \Deltah) * (density of air) * (g)

where

\small \DeltaP = pressure difference

\small \DeltaP = P1 - P2

\small \DeltaP = 101 kPa - 85 kPa

\small \DeltaP = 16 kPa

\small \DeltaP = 16000 Pa

\small \Deltah = difference in elevation between two points

g = gravitational constant of Earth = 10 m/s2

Substituting the values,

16000 Pa = (\small \Deltah) * (1.2 kg/m3) * (10 m/s2)

\small \Deltah = (16000 Pa) / [(1.2 kg/m3) * (10 m/s2)]

\small \Deltah = 1333.33 m

\small \Deltah = 1333.33 m * (3.28 ft / 1 m)

\small \Deltah = 4373.33 ft

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