Example — Barometric formula

The atmospheric pressure PP varies with altitude hh according to: dPdh=0,028gRTP=αP,\frac{dP}{dh} = -\frac{0{,}028\cdot g}{R\,T}\,P = -\alpha\,P, where g=9,81g=9{,}81 m/s², R=8,314R=8{,}314 J/(mol\cdotK), TT is the absolute temperature.

We separate: dPP=αdh\dfrac{dP}{P}=-\alpha\,dh, hence P(h)=P0eαhP(h) = P_0\,e^{-\alpha h}.

With T=293T=293 K: α=0,028×9,818,314×2931,13×104\alpha = \dfrac{0{,}028\times 9{,}81}{8{,}314\times 293} \approx 1{,}13\times 10^{-4} m1^{-1}. Therefore: P(h)=101325e0,000113h\boxed{P(h) = 101\,325\cdot e^{-0{,}000113\,h}} (with hh in metres, PP in Pascals).

Numerical example. At what altitude is the pressure half that at sea level? e0,000113h=0,5    h=ln20,0001136135 m.e^{-0{,}000113\,h} = 0{,}5 \implies h = \frac{\ln 2}{0{,}000113} \approx 6\,135\text{ m}. It is a reasonable result: at the summit of Everest, at about 88488\,848 m, the pressure is about a third of that at sea level.

Topics: Differential equations
Concepts: Decay · Barometric formula · Separable variables
Functions: Exponential function
Skills: Calculating · Integrating · Modelling