a.
\Find the angle
.
The equation is
.
Half-angle identity :
.
.
Since the mach number describing a plane
s speed cannot be negative,
.
b.
\Consider
.
Substitute the values of
in
.

The mach number of the plane is about 3.2.
\a.
.
b. The mach number of the plane is about 3.2.