Let's first look at Points 1a and
1b. Point 1a shows vTLM
determined using the E and I measurements and the transmission line
model expression. Point 1b shows the measurements of return
stroke velocity. The value of vTLM obtained
for
the
1985
experiment
2.07
does
not agree very well with the measured value 1.26.
This may be due to the complicated launch platform. Agreement was
a
little better for the 1987 experiment.
At Point 2 we can see that vTLM
using dE/dt and dI/dt is higher than the vTLM
determined using E and I. This discrepancy has not been
explained. The velocity values at Point 3 are appreciably higher
than any of the other values. This estimate of vTLM was
determined using dE/dt measured at 50 m distance from the triggering
point. As we mentioned earlier, these fields probably contain
induction and electrostatic field contributions and the transmission
line model expression should probably not be used with them.
We haven't explained the Eshoulder
column in the figure yet. A careful comparison of I and Erad
signals (which the transmission line model predicts should be
identical) shows some subtle differences between the two waveform
shapes. Rather than just a single peak, the Erad signal often has
a second somewhat smaller peak or shoulder as sketched below.
Much better agreement between vTLM and
measured velocities was obtained when the Eshoulder amplitude was used
with Ipeak in the transmission line expression when computing
vTLM.
Now we'll look at one possible explanation of the Eshoulder
feature (we mainly follow the discussion in the
Leteinturier
(1990)
paper mentioned earlier)
We ordinarily think of the return stroke as being a single
upward
propagating current that begins at the ground. This view is shown
in the figure above. Let's say a peak current of Io
at the ground produces a field with a peak value Eo at some
distance from the strike point.
It may be that the return stroke doesn't begin at the ground but a few
10s of meters above the ground at the junction point between the upward
connecting discharge and the stepped leader. In this case there
might not be just a single
upward propagating current, rather currents might travel up and down
from the junction point. The downward wave reaches the ground and is
partially reflected. This kind of a situation, together with a
few assumptions, can produce an E
field signal that resembles the peak and shoulder
features seen in the triggered lightning data.
The figure below provides some justification for starting the
return stroke above the
ground, i.e. at the junction point between the upward connecting
discharge and the bottom of the stepped leader channel. Positive
charge would tend to travel upward, negative charge downward.
This would result effectively in two upward pointing current
waves.
Let's follow this a little further. We'll assume that the current
rises to peak
value before the downward wave reaches the ground.
The waves
might travel at 1/3 the speed of light, 1 x 108 m/s.
If the
current peaks in 0.1 microseconds, the junction point would need to be
at least 10 m above the ground. If it takes 1 microsecond for the
current to reach peak the junction point would need to be 100 m high
(that seems a bit much).
A single upward propagating current with amplitude Io
will
produce a radiation field with amplitude Eo. What field will two
current waves each with amplitude Id produce? We need to find
some relation between Id and Io. To do that we need to look at
what happens when the downward traveling wave reaches the ground.
This is sketched in the figure below.
The top part of the figure shows the downward current
wave moving toward the ground. At the bottom of the figure we
show what happens when the wave reaches the ground. A portion of
the downward wave is reflected (shown in blue). We will assume
that the reflected current wave, which has amplitude R Id, and the
original wave, with amplitude Id,
add. So the total current
measured at the ground would be
and we are going to force Iground
to be equal to Io
so that from the point of
view of the
current
measured at the ground, the two versions of return stroke initiation (a
single upward propagating current wave that starts at the ground versus
upward and downward pointing current waves that start at a junction
point above the ground) are indistinquishable. The same current
waveform
would be measured at the ground in both cases.
Now that we can relate Id and
Io
we can go back to our earlier
figure
One current wave with amplitude Io produces a field Eo. Two
current waves, each with amplitutde Id, produce a field with a peak
value of n why the E field
from the 2 current waves peaks at 2Eo/(1+R).
So
we've
explained
part
of
the figure below (the amplitude of the E
field peak highlighted in yellow).
Now we need to explain
why the
field decreases and forms a shoulder and why the shoulder amplitude is
Eo. To do that we need to consider the unreflected portion of the
current wave.
The unreflected current
doesn't
just travel down into the ground as shown in the earlier figure.
It probably spreads out horizontally. In any event, as a field
emitter, it "turns off" and stops radiating (it is
traveling into a conductor). So we need to subtract its
contribution to the total E field.
So the descent from peak field to a shoulder field
occurs when the
downward current wave reaches the ground. A portion of the
downward current stops radiating field.
Let's go back to our summary of the results of the experimental
test of the transmission line model.
Much better agreement between transmission line model derived
velocities and measured velocities was obtained when the Eshoulder amplitude
was
used
instead
of
Epeak
in the
transmission line model
equation together with Ipeak. This
is particularly true for the 1987 experiment with its simpler launch
platform. Keep the 1.51 x 108
m/s velocity value in mind,
we'll
being referring to it again shortly in the final section in today's
notes.
We should note that we still haven't explained why a different vTLM was
obtained when using dE/dt and dI/dt data.
We'll end this lecture with a look at some experimental
measurements of distant
electric radiation fields and estimates of peak I and peak dI/dt values
that were derived from them. The measurements are described in
the publication cited below.
"Submicrosecond
fields
radiated
during
the
onset
of
first
return
strokes
in
cloud-to-ground
lightning,"
E.P.
Krider,
C.
Leteinturier,
and
J.C.
Willett,
J. Geophys. Res., 101, 1589-1597, 1996.
Here are some important points regarding this experiment.
1. Electric fields from lightning first return strokes 25
to 45 km away were
measured. Only the radiation field component is present at these
ranges.
Propagation between the strike point and the recording
station was entirely over salt water so that high frequency signal
content was largely preserved. The recording station was actually
one of the stations used in the triggered lightning experiment
described above (Point 2 on the map at the start of today's lecture)
2. The recording instumentation was triggered on an
RF signal rather than on E or dE/dt to prevent trigger bias.
The plot above shows range normalized dE/dt data versus
range. A set trigger threshold on an oscilloscope or waveform
recorder of some kind,
a fixed voltage, will correspond to larger and larger dE/dt values with
increasing range. Between about 40 and 80 km the distribution of
measured dE/dt signals will be biased toward
larger signal amplitudes. Only the green points on the plot above
which are above the
trigger threshold
would be recorded, beyond about 80 km very few of
the dE/dt signals wwould be large enough to trigger
the recording instrumentation. (This is a realistic but
fictitious data set being used for illustration).
The histograms below show the effect of trigger level bias on the
distribution of range normalized dE/dt measurements. The first
histogram plots the range normalized dE/dt measurements between 40 and
80 km which triggered the recording system. The mean value was 44
V/(m μsec).
The bottom histogram is the true distribution. I.e. it includes
the data that triggered the recording system and those that did
not. Including the latter group of data lowers the mean to 38
V/(m μsec).
The table below illustrates how measured dE/dt values can be range
normalized.
Three typical peak dE/dt values from return strokes at
ranges of
25, 35, and 65 km are shown in the left most column. We assume
the signals vary as 1/range. Data range normalized to 100 km are
shown in the right column.
3. Even though E field propagation was over salt water
some high frequency attentuation was still present. An atttempt
was made to correct for this.
The figure below shows the effects of propagation. The dI/dt
waveform used in the calculations is shown at the top of the figure.
The three lower plots show the dE/dt signal at 10, 35,
and 50 km
range. The signals are both attentuated and broadened (the
percentage refer to the pulse width at half maximum). The solid
line shows propagation over a perfectly conducting surface for
comparison.
And here are the main results from the experiment. First
the estimate of peak I derived from measured E amplitudes using the
transmission line model expression.
Note the value of the velocity used in the calculation
is the best
fit between measured I and E values in the experimental test of the
transmission line discussed earlier in today's class.
Next the estimate of peak dI/dt
Again the velocity from the experimental test of the
transmission
line model was used. Note the value used for dI/dt is different
from the value used to estimate peak I.
The estimate of average peak current compares well with values from
measurements made during strikes to instrumented towers that were
summarized in an earlier lecture. Those tower measurements
probably did not have sufficient time resolution to accurately record
peak dI/dt values. So the measurement above is one of the best
estimates of peak dI/dt in first return strokes available in the
literature.