document.write( "Question 788870: At constant temperature, the atmospheric pressure p (in Pa) at an altitude h (in m) is given by Ph = Poe^(-mgh/RT), where Po is the pressure where h = 0 (atmospheric pressure at sea level). Given that Po = 1013.25 hPa (atmospheric pressure at sea level) and Ph = 900 hPa, find the value of h.\r
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document.write( "Where P0 is the atmospheric pressure at some reference level
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document.write( "Ph is the atmospheric pressure at altitude h (m) above the reference level.
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document.write( "m is the molecular mass of air (0.0289644 kg/mol)
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document.write( "g is acceleration due to gravity (9.80665 ms-2)
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document.write( "R is the gas constant constant (8.314462 JK-1mol-1)
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document.write( "T is the temperature in Kelvin. In the lower altitudes temperature reduces with altitude at a rate of about 6.5 Kelvin per km of altitude. \n" );
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Algebra.Com's Answer #478670 by KMST(5328)![]() ![]() You can put this solution on YOUR website! \n" ); document.write( " \n" ); document.write( " \n" ); document.write( " \n" ); document.write( "Assuming that \n" ); document.write( " \n" ); document.write( "I do not have a temperature, so I will assume \n" ); document.write( " \n" ); document.write( "So the height is about 1,000 meters. \n" ); document.write( " |