### Video Transcript

A plane is flying at Mach 1.2. And an observer on the ground hears
the sonic boom 15 seconds after the plane is directly overhead. What is the altitude of the
plane? Use a value of 340 meters per
second for the speed of sound.

In this scenario, we have a plane
flying along at a steady altitude with a speed of 1.2 times the speed of sound,
which weβre calling π£ sub π . As the plane flies along, its
engines produce sound. And the sound waves from these
engines expand outward as time elapses. Since the plane is moving at a
speed greater than the speed of sound, that means that it creates a shock wave, a
line at which the sound waves produced by the plane stack on top of one another. This shock wave slowly moves
out. And weβre told that an observer on
the ground hears the shock wave 15 seconds after the plane is directly overhead.

Based on this and knowing that the
speed of sound is 340 meters per second, we want to solve for the altitude of the
plane, capital π΄. To solve for the attitude π΄, weβre
first gonna solve for the angle created by the shock wave and a horizontal line
through the center of the plane. Weβll call that angle π. And to solve for it, letβs consider
the triangle that π is a part of.

If we start at the center of the
first sound wave weβve drawn in and move from that center to the shock wave so that
the two lines meet perpendicularly, then we can say that the length of this line
weβve drawn in is equal to the speed of sound, π£ sub π , times the time elapsed,
what weβll call π‘. Likewise, we can draw a line
starting at that same center moving in a horizontal direction to the current
position of the plane and say that the length of that line segment is equal to π£,
the speed of the jet engine, times π‘, the time elapsed.

As we look at this right triangle
then, we see that π is related to π£ sub π times π‘ and π£ times π‘. In particular, we can write that
the sin of the angle π is equal to π£ sub π times π‘ over π£ times π‘. We see that the time values cancel
out from this fraction. And since π£ is equal to 1.2 π£ sub
π , that means our fraction reduces to one divided by 1.2. If we take the inverse sine of both
sides of this equation, we find that π is approximately equal to 56.44 degrees.

Now that we know π, letβs consider
how this can help us solve for the altitude π΄. With our diagram as shown, the
observer on the ground wonβt hear the shock wave until the shock wave has advanced a
bit further until itβs reaching the ground. When that takes place, weβll have a
right triangle with an angle π. And the side length opposite π is
the altitude π΄. In addition, the entire adjacent
side of this triangle is equal to the speed of our jet engine, π£, times the time
elapsed, π‘. This means we can once again use
the trigonometry of this right triangle to solve for what we want to find.

This time, we can say that itβs the
tangent of π which is equal to, in this case, π΄ over π£ times π‘. Rearranging, we can write that the
altitude of the jet is equal to its speed times the time thatβs elapsed since it was
overhead the observer times the tangent of the angle π, the angle its shock wave
makes with the horizontal. The speed, π£, is equal to the
speed of sound, 340 meters per second, times 1.2. The time, π‘, is equal to 15
seconds. And π as weβve seen is 56.44
degrees. Plugging all these values in to our
calculator, we find that, to two significant figures, π΄ is 9.2 kilometers. Thatβs the elevation of this plane
above ground level.