The atmospheric pressure is and altitude is
.
The rate of change of with respect to
is proportional to
.
Hence , where
is a constant.
At the sea level, the pressure is kpa.
Pressure at an altitude of is
kpa.
The general equation is .
Substitute and
in the above equation.
Substitute in the
.
Pressure at an altitude is
.
(a).
\Find the pressure at a altitude of .
Substitute in the pressure function
.
The pressure is kpa at an altitude of
.
(b).
\Find the pressure when altitude is m.
Substitute in the equation
.
The Pressure is kpa when altitude is
m.
(a) The pressure is kpa at an altitude of
.
(b) The Pressure is kpa when altitude is
m.