ATMO/ECE 489/589 Final Exam
May 9, 2017
Everyone should answer Question #1 (25 pts)
ATMO/ECE 489 students should then answer 3 of the remaining
questions (20 pts each)
ATMO/ECE 589 students should answer any 4 of the remaining
questions (20 pts each)
1. Please
answer any 5 of the following short answer questions (5 pts
each)
(a) Satellite observations indicate a
global lightning flashing rate of about 45
flashes/second. What would the corresponding global
flash density (flashes/(km2 year)) be?
(b) We might expect to measure an electric
field of 100 to 300 V/m at the ground during fair
weather. What if it were foggy outside, would you
expect to measure a higher, a lower, or the same value of
the electric field. Explain.
(c) Despite a sizable increase in population,
the number of people killed by lightning every year in the
United States has decreased from more than 400 in the
early 1900s to less than 30 people per year at the present
time (R.L. Holle, "Some Aspects of Global Lightning
Impacts," 2015 Amer. Meteorol. Soc. Meeting,
Phoenix). In addition to better hazard warning and
safety education, automobiles play an important role in
the decrease in lightning deaths. Why do you think
this is so?
(d) To calculate the
average score on an exam in a class like ours I would sum
up the exam scores and divide by the number of students,
i.e. I'd compute the arithmetic mean. With lightning
measurements such as peak return stroke current, the
geometric mean is often given instead of the arithmetic
mean. How do you compute the geometric mean?
Under what circumstances might the geometric mean better
characterize a group of measurements than the arithmetic
mean?
(e) List and
briefly discuss the sources of atmospheric ionization
present in (i) the lowest meter of the atmosphere, in
(ii) the first 10s and 100s of meters above the
ground, and (iii) between 1 and 10 km
altitude. Would the same list apply out
over the ocean?
(f) We generally assume that the electric
field at ground level is perpendicular to the earth's
surface. Why is that the case? Explain
also why, even though the earth is roughly spherical,
we generally write the E field at the ground as having
a z-component (Ez) rather than a
radial component (Er).
(g) The transmission line model (TLM) is
widely used to estimate peak return stroke current and
current derivative values from distant measurements of
electric and magnetic radiation fields. What is
the actual TLM relationship between peak current
and peak field (or peak current derivative and peak
field derivative value)? What assumptions are
made when deriving the transmission line model
equations.
(h) I
don't remember having mentioned
dry lightning, ribbon lightning, bead lightning, heat
lightning, or hot lightning in class this
semester. What is meant by these terms or
descriptions? Are these really
different types of lightning? (this was covered
in Spring 2015, on Feb.
27 as a matter of fact).
(i) People standing at points A and
B in the figure below are about the same distance from
where lightning has struck the ground. Would the
thunder they hear be about the same or
different? If different, in what way(s)?
2.
Aircraft are struck by lightning fairly
frequently. The discharge is often triggered by the airplane
itself and there have been several field campaigns that sought to
better determine the conditions that could
lead to a lightning trigger and to evaluate whether aircraft
were adequately protected from a lightning strike.
You'll find a supplementary reading section on "Lightning
interactions with aircraft" in this semester's lecture notes.
The aircraft in those research studies made measurements of the
surrounding thunderstorm electric field. Field mills are
mounted at multiple locations on the aircraft body and a complex
analysis procedure is used to determine the 3-dimensional field
surrounding the aircraft and also to account for any charge that
might have built up on the aircraft. The locations of 5
field mills on the Convair CV580 and the Transall C160 are shown
below
This question will make use of a much simpler geometry, a
conducting sphere, and will assume the sphere is placed in a
uniform, vertically oriented, ambient electric field (the aircraft
studies generally assume that the field is uniform but of unknown
orientation).
In our Thursday,
Feb. 2 class, we derived the potential function,
Φ(r,θ) in the space surrounding a sphere
The problem geometry is shown above. The
potential function that we ended up with is shown below
One of the boundary conditions that we used when working out
the problem was that the potential was constant on the surface
of the sphere, that is the case above when r = a. Now we
will imagine that the sphere is charged. The potential
function for a point charge is
We'll add this expression to the equation above for
the uncharged sphere and end up with an expression for a
charged sphere in a uniform field (here's
a reference that convinced me this is a valid approach)
(the Φo term was dropped in this
expression). Note that Φ is constant on the
surface of the sphere in this case also (r = a in the
expression above).
This Final Exam question has three parts:
(a) The charge on the sphere is spread out over the
surface of the sphere. Using the expression above show
that the surface charge density on the surface of the sphere
is
(b) Integrate this expression for surface charge density over
the surface of the sphere
(c) Imagine you were able to measure the electric field at the
top and bottom surfaces of the sphere (just as field mills are
able to measure the electric field at various locations on an
aircraft). Show how you could use the measurements of Etop
and Ebottom to determine both the ambient field, Eo,
and the total charge, q, on the sphere.
3. A negatively
charged, downward propagating stepped leader is approaching flat
ground. About how high above the ground will the tip of the
leader be at the moment upward connecting discharges are initiated
at the ground and begin to move upward to intercept the
leader? You can assume that a peak current of 45 kA is
measured in the ensuing return stroke once attachment between the
leader and one of the upward connecting discharges is made.
4. The point charge Q in the figure below is positioned a
distance H above the ground (which you should assume is a
conducting surface). The electric field is being measured
a distance D away.
(a) Derive an expression for the
electric field as a function of H/D.
(b) Show that the electric field reaches a maximum
when H/D = 1/√2
5.
Orthogonal components of the magnetic field have
been measured at two locations in a network of magnetic
direction finders. Station #1 has arbitrarily been placed
at the origin of the x-y coordinate system. Station #2 is
located to the northeast of Station #1 as shown below. You
can ignore any attenuation of the field amplitudes by
propagation and can assume the ground is flat.
(a) Determine the bearing vector from
each station to the lightning strike point.
(b) Determine the x, y coordinates of the strike point
(c) What is the range normalized amplitude (100 km) of
the B field (magnetic field)?
6. Starting with the
Ohm's law equation and the differential form of Gauss' Law
show that the n+ and n- small ion
concentrations vary with altitude as follows:
B+ and B-
are the positive and negative small ion mobilities, and e is
the charge on an electron. You can assume the J and E
are functions of z only. Note also that while we mostly
assumed that n+ and n- were
equal during much of the semester, that is not the case here.
7. How much
charge will appear on the flat plate electric field antenna
shown below when exposed to a negative (downward pointing)
electric field of 200 V/m? What voltage will appear
across the 100 pF capacitor shown in the circuit below?