A thermodynamic equation for pressure as a function of altitude, z, is
P(z) = P0 [(T0 - Γ z)/T0]p
where Γ is the adiabatic lapse rate (~ .0098 °C/m) , T0 is the temperature (in Kelvins) at the surface and P0 is the pressure at the surface.
the exponent p is ~ 3.5 and p ~ 0.029 x 9.81/( R Γ)
{ R is the gas constant ~ 8.3 and 0.29 is the effective molar mass of air in kg}
According to the problem statement, the ratio of pressure at Denver to that at sea level is 12.15/14.7 = .827 . To get the formula to work out (with z = 1609 m at Denver), we need
.827 =[ (T0 - 1609 x .0098)/T0 ]3.5 which implies that [(T0 - 15.8 )/ T0] = .947 So, solving for T0, yields T0 = 298 K. This is a reasonable number.
At Mexico City z = 2225 m. [(298 - 21.8)/298 ]3.5 = .767 So the pressure at Mexico City is .767 x 14.7 = 11.3
The calculation for Mt. Everest is similar.
Erica T.
y = 14.7(0.999964)^x??? But where did 0.999964 come from
Report
05/04/15
Erica T.
05/04/15