The air layer of thickness Δx at a distance x form the front of the cabin experiences the force of pressure
[p(x+Δx)−p(x)]S,
where S is the cross-sectional area of the cabin SInce air is at rest relative to the cabin, the equation of motion for the mass of air under consideration has the form
ρSΔxa=[p(x+Δx)−p(x)]S
Making Δx tend to zero, we obtain
dpdx=ρa
whence
p(x)=p1+ρax
Since the mean pressure in the cabin remains unchanged and equal to the atmospheric pressure ρ0 the constant p1 can be found from the condition
p0=p1+ρal2,
where l is the length of the cabin. Thus in the middle and near parts of the cabin, the pressure is equal to the atmospheric pressure, while in the front and rear parts of the cabin, the pressure is lower and higher than the atmospheric pressure by
Δp ρal2≃0.03 Pa respectively