In this lecture we will look at how E field measurements at the
ground can be used to determine the locations and amounts of
charge involved in lightning discharges. Then we'll look at
some of what has been learned from these types of studies.
The data and results
that we will be discussing come largely from
experiments conducted at the Kennedy Space Center
(KSC). A large (15 km x 25 km) network of
electric field mills is operating at KSC to identify
and warn of thunderstorm and lightning hazards.
The pre-1995 configuration of the field mill network
is shown in the figure below (source of this and the
following three figures: J.M.
Livingston
and
E.P.
Krider,
"Electric
Fields
Produced
by
Florida
Thunderstorms,"
J. Geophys. Res., 83, 385-401, 1978). The
network was upgraded in 1995.
The network that was operating up to 1995 had 0.1
second time resolution. That is fast enough to
resolve a lightning flash, but not the individual
return strokes that make up cloud to ground
flashes. The dynamic range was -15 kV/m to +15
kV/m and E field signals were digitized with 30 V/m
accuracy. The overall accuracy of an individual
field mill was about 10%.
Examples of fields recorded during 6 small
storms. Storms in this category lasted from
35 up to 85 minutes. Individual storms
produced 16 to 82 discharges. The maximum
flashing rate during a small storm is 1
flash/minute.
A single example of a large storm E field
record is shown below
Storms like this are often broken into
initial, very active, and
end-of-storm-oscillation portions. Note
the very slow but large amplitude oscillations
in the final EOSO portion.
Large storms in the Livingston and Krider
study had durations ranging from 75 to 265
minutes, produced 515 to 1212 discharges, and
maintained flashing rates of 5 to 10 flashes
per minute for 50 to 90 minutes. Number
of flashes per 5 minute interval in a
representative large storm are shown in the
histogram below.
It turns out we really won't be analyzing
electric fields measured at the ground, rather
the field changes, ΔE. The figure below
explains why this is the case.
Fields measured at the ground usually have
lower amplitudes than fields measured just a
100 or 200 meters above the ground.
Fields at the ground probably wouldn't exceed
10 kV/m; fields just a few hundred
meters above the ground could be several times
larger. The field changes
measured at the ground and aloft are the same.
As the field at the ground begins to build
after a lightning discharge, corona discharge
from pointed objects and vegetation "sprays"
space charge into the air above the
ground. This limits the amplitudes of
fields seen at the ground and affects the
shape of the field recovery between
flashes. We can't really get an accurate
measurement of the thunderstorm field at the
ground. You can, however, get an
accurate measurement of the field change at
the ground (it occurs so quickly that space
charge can't be created or move quickly enough
to affect the field change value).
Now lets start to look at what can be done
when field change measurements are made at
multiple locations on the ground.
We'll consider the simplest model of a
cloud-to-ground discharge and assume that the
charge neutralized by the flash comes from a
uniform sphere of charge in the cloud.
You can treat this as a single point charge
(Point 1). Our objective will be to use
the delta E measurements to determine the
location (x, y, and z coordinates) and
magntitude of the neutralized charge (ΔQ).
We show the location of one of the field mill
sites in the figure. At that location we
will have a measurement of the field change, ΔEmi.
We can also calculate the field change that
the charge neutralized at Point 1 would
produce at Point 2, the location of
the ith
field mill site. The expression for this
calculated field change is shown below.
We're trying to determine ΔQ,
x, y, and z. How can we
calculate ΔEci
if we don't know what they are? We
make an initial guess about the location and
the amount of charge neutralized during the
lightning discharge. And we
have field change measurements and can
calculate field changes at the other field
mill sites. We can adjust
the values of x, y, z, and ΔQ
until the chi-squared function below is
minimized. That will give us our best
estimate of ΔQ and its
location.
This first histogram gives solutions for ΔQ,
the (negative) charge carried to ground in 70
cloud to ground discharges.
The next histogram shows that this
charge was largely found between 6 and 9 or 10
km altitude.
Note that this corresponds to a -10o to -30o or -35o C
temperature range (the -10o to -30o
C range is highlighted above).
Finally the figure below shows that
75% of cloud-to-ground discharges strike the
ground at a distance, D, of 5 km (3 miles) or
less from the center of the charge neutralized
by the flash. 95% of the discharges
strike the ground within 8 km (5 miles) of the
charge center. The distance D is defined
in the figure below at right.
You would generally expect the field change
amplitude to get larger as you get closer to a
storm. We pointed out earlier however
that the field amplitude is sometimes
surprisingly small when you are very close to
a storm. The field change may also
switch polarity.
These
observations suggest that a lower volume
of positive charge might be involved in
cloud-to-ground discharges. This led
to the development of a 2 charge model,
illustrated below.
This
is the most general form of the two
charge model - the two charges can
have different magnitudes and can have
completely different locations in
space. A variation on this is
the point dipole model where the two
charges are of equal amplitude but
opposite polarity. Another model
assumes the two charges are aligned
vertically. The calculated field
change expression now contains 8
unknowns (ΔQ1,
x1,
y1,
z1,
ΔQ2,
x2,
y2,
and z2).
Again you use pairs of measured and
calculated fields and minimize a
chi-squared function to determine the
optimal solution for these charge and
location variables.
The next two figures shows some of the
results obtained with this arbitrary 2
charge model (source: M.J. Murphy, The
Electrification of Florida
Thunderstorms, PhD Dissertation, Univ.
of Az., 1996)
The
circles indicate charge
neutralized during lightning
discharges, time and altitude are
plotted along the horizontal and
vertical axes, respectively.
Cross hatched circles are positive
charge, open circles are negative
charge. The radius of the
circle is proportional to the
amount of charge neutralized.
Both intracloud and cloud to
ground discharges were occurring
during this storm. An
example of each is shown.
Intracloud discharges involve
positive charge in the main
positive charge center located in
the upper portion of the
thundercloud and negative charge
in the main negative charge center
in the middle of the cloud.
Cloud-to-ground discharges
neutralize negative charge
in the middle of the cloud and
almost always involve some
positive charge in one of the
lower positive charge
centers. The vertical dotted
lines at the bottom edge of the
figure indicate cloud-to-ground
discharges detected and located by
the National Lightning Detection
Network.
The next figure is from a
little more active thunderstorm
cell.
There seems to be a tendency
for the amounts of
charge neutralized in discharges
to increase with time (larger
diameter circles toward the end of
the storm). The
altitudes of the positive charges
neutralized in intracloud
discharges seem to move to higher
altitudes in the middle and later
portions of the storms.
The chi-squared procedure for
determining charge center
locations and charge magnitudes
using multi-station field change
measurements has also be used with
slow E field antenna
systems. Slow E records have
faster time resolution and can
accurately record the field
changes produced by the separate
return strokes in a cloud to
ground flash. The results we
looked at above were derived from
field mill records and were an
integration of all the processes
that occur during a flash.
The antenna sensor plate is
mounted about 1 m above the ground
and is surrounded by a culvert
(probably to keep cattle and
wildlife away from the
antenna. The decay time
constant of the integrating
electronics was 10 seconds.
It is worth pointing out that,
because the antenna plate is not
mounted flush with the ground, its
effective area will be greater
than its geometric area.
The effective crossectional
area of a sensor plate positioned
above the ground is greater than
its geometrical crossection.
Some of the E field lines that
wouldn't strike a plate mounted
flush with the ground curl around
and strike the sides or bottom of
a plate positioned above the
ground. The effective area
would need to be determined by
calibration.
The antenna network was installed
near Socorro, New Mexico.
An example of a CG flash slow E
field record is shown in the
figure below. Six return
strokes have been identified.
A stepped leader field change
can be clearly see on several of
the records and has been
highlighted in yellow. The
slow field change that follows the
last return stroke is caused by a
continuing current and has been
highlighted in pink.
The figure below shows
locations of the charges
neutralized by the separate return
stroke in 4 cloud-to-ground
flashes. Flash 9 has been
highlighted because those are the
charge locations determined using
the slow E field data shown
above. Charge tapped by the
continuing current that followed
the 6th return stroke in Flash 9
has been highlighted in pink.
In
each case successive return
strokes tap separate volumes
of charge that are further and
further away from the staring
location.