Radar detection of individual raindrops
Jerome M. Schmidt; Piotr J. Flatau; Paul R. Harasti; Robert. D. Yates; David J. Delene; Nicholas J. Gapp; William J. Kohri; Jerome R. Vetter; Jason E. Nachamkin; Mark G. Parent; Joshua D. Hoover; Mark J. Anderson; Seth Green; James E. Bennett
Schmidt, J.M., P.J. Flatau, P.R. Harasti, R.D. Yates, D.J. Delene, N.J. Gapp, W.J. Kohri, J.R. Vetter, J.E. Nachamkin, M.G. Parent, J.D. Hoover, M.J. Anderson, S. Green, and J.E. Bennett. Radar detection of individual raindrops. Bulletin of the American Meteorological Society, 100(12):2433–2450, 2019.
Abstract
Descriptions of the experimental design and research highlights obtained from a series of four multiagency field projects held near Cape Canaveral, Florida, are presented. The experiments featured a 3 MW, dual-polarization, C-band Doppler radar that serves in a dual capacity as both a precipitation and cloud radar. This duality stems from a combination of the radar’s high sensitivity and extremely small-resolution volumes produced by the narrow 0.22° beamwidth and the 0.543 m along-range resolution. Experimental highlights focus on the radar’s real-time aircraft tracking capability as well as the finescale reflectivity and eddy structure of a thin nonprecipitating stratus layer. Examples of precipitating storm systems focus on the analysis of the distinctive and nearly linear radar reflectivity signatures (referred to as “streaks”) that are caused as individual hydrometeors traverse the narrow radar beam. Each streak leaves a unique radar reflectivity signature that is analyzed with regard to estimating the underlying particle properties such as size, fall speed, and oscillation characteristics. The observed along-streak reflectivity oscillations are complex and discussed in terms of diameter-dependent drop dynamics (oscillation frequency and viscous damping time scales) as well as radar-dependent factors governing the near-field Fresnel radiation pattern and inferred drop–drop interference.
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Radar Detection of Individual Raindrops 1
2
Jerome M. Schmidt1, Piotr. J. Flatau2, Paul R. Harasti1, Robert. D. Yates3, David J. 3
Delene4, Nicholas J. Gapp4, William J. Kohri5, Jerome R. Vetter5, Jason E. Nachamkin1, 4
Mark G. Parent6, Joshua D. Hoover7, Mark J. Anderson7, Seth Green7, and 5
James E. Bennett8 6
7
1Marine Meteorology Division, Naval Research Laboratory, Monterey CA 8
2Scripps Institution of Oceanography, University of California, San Diego, CA 9
3AECOM, Dahlgren, VA 10
4The University of North Dakota, Grand Forks, ND 11
5The Johns Hopkins University Applied Physics Laboratory, Laurel, MD 12
6Radar Division, Naval Research Laboratory, Washington, DC 13
7Naval Surface Warfare Center Dahlgren Division, Dahlgren, VA 14
8The Naval Ordnance Test Unit, Cape Canaveral, FL 15
16
Corresponding Author: Jerome M. Schmidt, Marine Meteorology Division, Naval Research 17
Laboratory, 7 Grace Hopper Ave, Monterey, CA, 93943 18
Email: jerome.schmidt@nrlmry.navy.mil 19
20
Early Online Release: This preliminary version has been accepted for
publication in Bulletin of the American Meteorological Society, may be fully cited,
and has been assigned DOI The final typeset
copyedited article will replace the EOR at the above DOI when it is published.
© 2019 American Meteorological Society
10.1175/BAMS-D-18-0130.1.
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Abstract 21
Descriptions of the experimental design and research highlights obtained from a series of four 22
multi-agency field projects held near Cape Canaveral, FL, are presented. The experiments 23
featured a 3MW, dual polarization, C-band Doppler radar which serves in a dual capacity as both 24
a precipitation and cloud radar. This duality stems from a combination of the radar’s high 25
sensitivity and extremely small resolution volumes produced by the narrow 0.22 degree 26
beamwidth and the 0.543 m along-range resolution. Experimental highlights focus on the radar’s 27
real-time aircraft tracking capability as well as the fine-scale reflectivity and eddy structure of a 28
thin non-precipitating stratus layer. Examples of precipitating storm systems focus on the 29
analysis of the distinctive and nearly linear radar reflectivity signatures (referred to as “streaks”) 30
that are caused as individual hydrometeors traverse the narrow radar beam. Each streak leaves a 31
unique radar reflectivity signature that is analyzed with regard to estimating the underlying 32
particle properties such as size, fall speed, and oscillation characteristics. The observed along-33
streak reflectivity oscillations are complex and discussed in terms of diameter-dependent drop 34
dynamics (oscillation frequency and viscous damping time scales) as well as radar-dependent 35
factors governing the near-field Fresnel radiation pattern and inferred drop-drop interference. 36
Capsule Summary: A high resolution, hybrid cloud and precipitation radar reveals the 37
fascinating structure and behavior of individual hydrometeors within observed cloud systems. 38
39
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Introduction 40
41
At first glance, the discrete detection of individual raindrops using either surface or airborne 42
radar platforms would seem to be an impossible und ertaking. Calculations using standard 43
Marshall and Palmer (1948 ) type size distributions, after all, would suggest precipitation sized 44
particle concentrations on the order of 1000 m -3 even in light rainfall conditions of only 2 .0 mm 45
hr-1. Such concentrations would easily translate into over a billion or more precipitation sized 46
particles within modern day WSR-88D operational radar resolution volumes (on the order of 10 6 47
m-3) that stem from this radar’s 250 m range resolution and 0.925 degree beamwidth (see Table 48
1). Inferences on the internal cloud structure derived from remote s ensing using even higher -49
resolution research radars have thus long relied, with great success, on the statistical properties of 50
the returned microwave signal to extract critical particle characteristics such as the particle habit, 51
phase, and canting angle (Seliga and Bringi 1976; Illingworth et al. 1987; Zrnić et al. 1993; Orr 52
and Kropfli 1999; Bringi and Chandrasekar 2001; Matrosov et al. 2001; Houze 2004; Houser and 53
Bluestein 2011; Matrosov et al. 2012; Chandrasekar et al. 2013, Hubbert et al. 2018). 54
55
The more elusive undertaking of single particle detection to date has lar gely been relegated to 56
highly idealized environmental settings. Early r adar studies of indiv idual hydrometeors were 57
attempted by Atlas et al. (1960) and Willis et al. (1964) who studied the returns from large hail 58
stones tethered to or released from weather balloo ns. More cont rolled studies have been 59
conducted in laboratory wind tunnels where individual raindrops could be suspended in the air 60
stream for prolonged periods of time. Drop properties, such as the natural drop oscillation 61
frequencies, could then be recorded using photographic techniques and microwave 62
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measurements (Brook and Latham 1968 ). Additional studies over the past several decades have 63
provided detailed insight on the factors impacting the drop shape, canting angle, oscillation 64
frequencies, viscous damping time scales, and fall s peed characteristics (Rayleigh 1879; Gunn 65
1949; Blanchard 1950; List and Hand 1971 ; Musgrove and Brook 1975; Pruppacher and Klett 66
1978 [pgs 315-322]; Beard et al. 1983; Beard 1984; Beard and Kubesh 1991; Testik et al. 2006; 67
Szakáll et al. 2010). 68
69
A series of specialized experiments utilizing an advanced ground-based radar operated by the 70
U.S. Navy have demonstrated that it is now possible to extend the studies of individual raindrops 71
beyond the wind tunnel to observed precipitating cloud systems (Schmidt et al. 2012) . The 3 72
MW, C-Band, dual-polarization Mid-Course Doppler Radar used in that study (hereafter referred 73
to as the MCR; Fig. 1) has a maximum radar resolution volume on the order of 14 m3 at a range 74
of 2 km from the radar (a comparison of the MCR attributes to other well -known radars is 75
provided in Table 1). The MCR makes the observations of individual raindrops more tenable 76
provided they exceed the radar’s minimal detectable diameter at a given range [Dmin > 0.4 mm @ 77
2 km when the drops are embedded in a background reflectivity field of -40 dBZ; see Schmidt et 78
al. (2012) for details]. 79
80
The CAPE Field Experiments 81
82
The MCR-derived raindrop signatures were first observed in 2009 during the second of four field 83
experiments held bet ween 2008 and 2015 (Table 2). The original purpose of these experiments 84
was to assess the feasibility of using the MCR for basic cloud research and model validation 85
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applications. Historically, the MCR had been utilized up to 2011 to study the debris field 86
associated with the NASA Space Shuttle launches in the return -to-flight missions after the 1986 87
Challenger disaster. A subsequent effort to incorporate the MCR for cloud studies initially gre w 88
from a small group of scientists and rad ar engineers in 2008 to a much larger multi -agency 89
research effort by 2015. Each follow-on experiment in the series included additional instruments 90
to help guide the placement of the research aircraft and the MCR’s specialized higher -resolution 91
waveforms (Fig. 2 and Table 2). 92
93
The MCR is a dual polarization linear frequency modulated (LFM) pulse compression radar that 94
transmits at a pulse repetition frequency (PRF) of either 160.1 or 320.2 Hz. When used at the 95
lower PRF, the MCR typically transmits two wave forms (every other pulse) each of which have 96
a right-hand circular polarization and a one-way 3 dB far-field beamwidth of 0.22°. A quadratic 97
phase modulation is applied to the transmitted pulse which, after the 2010 radar upgrade, covers 98
a swept frequency bandwidth (B) of either 8.0 or 500 MHz (subsequently referred to as the 99
narrowband and wideband waveforms, res pectively). A matched filter data processing technique 100
is applied to the received signal and this leads to 6 dB range resolution values (R6 = Gc/2B) of 101
34.02 and 0.543 m for the narrowband and wideband waveforms, respectively [where c is the 102
speed of light (m s -1) and G is the normalized 6dB width that has a value of either 1.812 103
(wideband) or 1.816 (narrowband)]. The MCR’s high 3MW transmit power and large 15.24 m 104
diameter dish help overcome the loss in sensitivity that can otherwise arise in radars which 105
transmit at longer wavelengths (Kollias et al. 2016). When combined with the other radar 106
attributes noted above, the MCR maintains a relatively high sensitivity in comparison to other 107
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well established cloud and precipitation radars ( Table 1). It is th is combination of factors which 108
thus help make the detection of individual hydrometeors possible within the free atmosphere. 109
110
The wideband and narrowband waveforms are each comprised of two range windows that are 111
300 m and 75 km in length, respectively. These range windows can be placed contiguously or in 112
separate range locations of the MCR’s boresight direction at any given time. When located closer 113
to the radar, the range windows can fall within the radar’s near-field or Fresnel region where 114
both amplitude and phase ripples may be present in the transmitted waveforms. These ripples can 115
be of significance in the analysis of individual hydrometeors as they can introduce oscillations in 116
the extracted particle time series that can impact the interpretation of the derived spectral 117
analysis. Based on the MCR’s 15.24 m dish diameter and transmitted 0.053 m wideband 118
wavelength, the Fresnel region is calculated to lie between the ranges of 0.160 and 8.76 km and 119
thus encompasses the location of the wideband observations shown later in the text. 120
121
The MCR’s radiation pattern in the Fresnel region was obtained numerically using the GRASP 122
Software (TICRA, Copenhagen, Denmark, www.ticra.com), which is the industry standard for 123
analyses of electromagnetic radiation emitted from large reflector antennas [see Appendix A for 124
details]. The numerical results are shown at a range of 1.9 km in Fig. 3 as this location 125
corresponds closely with the level of the primary wideband observations shown later in the text. 126
The simulated cross-beam amplitude and phase patterns are symmetric about the center of the 127
domain and appear to lack significant amplitude or phase ripples near the radar boresight (Fig. 128
3). There is a subtle weakness in the amplitude and phase gradient fields evident at ranges of 10 129
to 15 m from boresight and this is a result of a ripple on the transmitted pulse that appears nearly 130
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20 dB down from the peak (Fig. 4). The cross-beam structure evident in Fig. 4 indicates that the 131
Fresnel region beam structure is slightly wider than otherwise assumed for the far-field 132
beamwidth change introduces a bias in our calculated returns which we estimate to be on the 133
order of 0.7 dBsm (see Appendix A for details). The possible impact of the main amplitude and 134
phase ripple will be addressed later in the text when the structure and significance of the 135
individual particle spectra are discussed. 136
137
The MCR incorporates a number of standard scanning strategies including vertical stares, Range 138
Height Indicator ( RHI), Plan Position Indicator ( PPI), and volume scans. To date, these scans 139
have been applied to document the structure of cirrus clouds, deep convective systems and their 140
associated stratiform cloud shields, mammatus clouds (Fig. 2), altocumulus cloud layers, low -141
level stratus, and multiple cases where individual raindrops were detected by the ra dar. The 142
MCR’s relatively small Nyquist interval (±λPRF/4 = ±2.1 m s-1) can hamper the analysis but this 143
has not been a significant issue to date in our studies of shallow statiform or cirrus cloud layers. 144
Velocity aliasing issues can arise , however, in the studies of deeper convective clouds or below 145
the melting layer of precipitating stratiform cloud systems. In such cases, we use the boot -146
strapping techniques of Bargen and Brown (1980) as well as independent Doppler information 147
provided by the METEK Mi cro Rain Radar to help unfold the Doppler velocities into the 148
appropriate Nyquist interval. 149
150
Finally, the MCR also has a special scan that can be used to track research satellites [such as the 151
A-train; Stephens et al. (2002)] or research aircraft in real-time (Fig. 5a,b). These scans will be 152
used to improve the MCR derived Z-LWC relationships and understanding of the internal cloud 153
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properties using the co-located radar and in situ cloud observation (Fig. 5c,d). The presence of 154
liquid water and chain-like crystals composed of large frozen drops in sub -40° C conditions 155
within Florida anvil systems are of particular research interest (Fig. 5c,d). Such crystal types are 156
not frequently observed but are thought to be influenced by the cloud electric field (Gayet et al. 157
2012). Plans for our pending 2019 field study include additional instruments, such as the aircraft-158
based electric field measurements, to gain additional insight into the environmental factors 159
governing the development of these chain-like crystals. 160
161
Detection of Individual Hydrometeors 162
163
The MCR radar signatures attributed to the presence of individual hydrometeors were first 164
recorded during scans of a deep convective storm system observed on the final day of the 2009 165
field study (Fig. 6). Two regions where the wideband recorded unusual radar reflectivity patterns 166
within this storm system are given by the location of the two boxes labeled B1 and B2 in Fig. 6. 167
The reflectivity data shown in B1 were associated with a transient cell that passed over the radar 168
between 2149 and 2154 UTC (Fig. 7). Note the rapid transition in the reflectivity pattern that 169
occurred near 21:49:30 UTC as a series of short-lived and discrete reflectivity anomalies that 170
suddenly appear against the otherwise more uniform background reflectivity field. The 171
anomalies were randomly orientated in space and time and indicative of multiple inbound and 172
outbound “targets”. A second set of anomalies derived from B2 were associated with a vertically 173
oriented precipitation streamer that originated much higher in the parent cloud system (labeled 174
R1 in Fig. 6). In this case, the B2 anomalies all had linear structures indicative of inbound 175
targets exclusively (Fig. 8). These anomalies are evident within R1 and can be seen as well both 176
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entering and exiting this feature along its lateral flanks suggesting the two features are possibly 177
linked. These transient reflectivity anomalies would later be recognized as the first MCR 178
measurements of individual cloud hydrometeors. Given their linear nature and relatively “bright” 179
reflectivity returns, these features were subsequently dubbed “radar streaks” by Schmidt et al. 180
(2012). 181
182
The unexpected appearance of the radar streaks in the final few moments of the 2009 field 183
campaign led to a concerted effort to replicate the observations in subsequent field programs. 184
Improvements were made to the MCR waveforms after 2009 in order to reduce the magnitude of 185
the range sidelobes, from 15 to 35 dB down from the peak. This was accomplished through the 186
application of more accurate phase compensation tables and post-processing waveform 187
equalizers. This was undertaken to reduce the anomalous reflectivity “shadows” found to arise 188
on both sides and parallel to particularly strong streaks evident in the 2009 data set (Fig. 7). The 189
wideband range windows were also subsequently extended from 150 m to 300 m after 2010. 190
Taken together, these changes now provide a much better opportunity to observe clean streak 191
patterns associated with the developing rain shafts and vertical velocity patterns over a much 192
deeper layer of the parent storm system (Fig. 9). 193
194
By further limiting the temporal and spatial scales of the wideband plots, one is able to discern 195
the radar signatures associated with each individual streak (Fig. 10). The bulk streak properties 196
related to their magnitude, slope, and duration can be used to estimate the particle size and the 197
translational and radial velocity of the particles as they enter and then exit the beam. These 198
properties can be impacted by a variety of factors that depend on the particle’s precise trajectory 199
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through the beam, the storm’s vertical velocity pattern, the mean and turbulent structure of the 200
environmental flow and possibly drop-induced lateral drift which Testik et al. (2006) have shown 201
can be as high 1-2 m s-1. Based on the streak slopes and the radar cross section (RCS) values 202
evident in Fig. 10, one infers a net radial motion toward the radar of 4.9 to 5.7 m s-1 and particle 203
size estimates in the range of 2.9 to 3.5 mm (see Appendix A for details). As particles at this 204
altitude and size range should have terminal velocities on the order of 8.8 to 9.4 m s-1 (Beard 205
1976), the slower slope-based velocity estimates suggest the particles are embedded in updraft on 206
the order of 4 m s-1 (confirmed through a separate Doppler analysis not shown). 207
208
The data shown in Fig. 10 also reveal interesting variations in the along-streak temporal trends 209
for each particle. The pulse-to-pulse along-streak RCS time series extracted for S2, S3, and S5 210
highlight some of the apparent variability between particles (Fig. 11). The mean parabolic 211
temporal trends evident in each time series results from the movement of the particles across the 212
vertically orientated beam. The magnitude of the perturbations about these mean trends was 213
greatest in the highly periodic S2 time series (Fig. 11a). The corresponding spectral analysis of 214
the S2 perturbations indicates these oscillations were centered about a broad peak in frequency 215
near 26 Hz and a secondary maximum near 53.7 Hz (Fig. 12a). Similar higher amplitude and 216
periodic fluctuations were also evident in S3 but these oscillations rapidly dampened in time as 217
the particle began to recede from its closest approach to the beam boresight (Fig 11b). The e-218
folding reduction in the perturbation amplitude for S3 was well-observed and occurred over a 219
time-scale of approximately 0.3 seconds. The spectral plot for S3 indicates a strong contribution 220
near 38 Hz arising during the initial portion of the transect and weaker contributions below 25 221
Hz and near 60 Hz (Fig. 12b). The S5 perturbations were of intermediate magnitude throughout 222
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(Fig. 11c) with several spectral peaks arising at different points along the transect (Fig. 12c). The 223
weaker fluctuations of S5 were similar to those found for the S1 and S6 streaks (not shown) 224
while those of S4 compared more favorably with that shown for S3. 225
226
Streak Analysis and Discussion 227
228
The ability to observe individual hydrometeors with radar naturally leads one to question 229
whether the along-streak data can be further analyzed in order to bring out additional particle 230
characteristics. The calculation of the natural vibrational and viscous damping characteristics as 231
a function of drop size might be two of many such parameters as each process occur over time-232
scales far less than that needed for a given streak to cross the beam (Brook and Latham 1968; 233
Beard et al. 1983). Isolating cause and effect can be difficult to undertake in practice, however, 234
due to nuances in the radar itself such as Fresnel region effects, possible sidelobe contamination, 235
the uncertainty of the drop’s position within the beam, or multi-particle interactions such as 236
described by Doviak et al. (1979). Additional physical processes are also likely to arise in 237
observed cloud systems such as drop-drop collisions, wake vortex shedding, multi-modal drop 238
vibrations, or turbulence induced fluctuations among others (Beard and Kubesh, 1991; Szakáll et 239
al. 2009). 240
241
An important initial concept in the analysis of individual hydrometers is that of determining the 242
radar’s minimum detectable particle size. For the MCR, this relationship is governed by an 243
expression of the form shown in Eq. A2 which is governed by the range to the particle, the 244
particle size and phase, and the magnitude of the particle and background signal to noise ratios. 245
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The relationship is illustrated by the curves shown in Fig. 13 which indicate that the minimum 246
detectable particle size increases as the background reflectivity and the range to the target 247
increase. Particles easily identified in Fig. 8 along R1’s lateral flanks, where the background 248
reflectivity is weak (~ -20 dBZ), thus become much more difficult to discern within R1 where 249
the background reflectivity values are much higher (~10 dBZ). This is akin to the faintest stars 250
being the first objects to fade from view as daybreak ensues along the morning horizon. For the 251
conditions shown in this paper, particle sizes of 1 to 3.5mm would have been required for the 252
streaks to stand out against the observed background reflectivity values (Fig. 13). Rising 253
background reflectivity values also mean that particles must pass closer to boresight before they 254
exceed the minimum detection threshold. For conditions shown in this study, particles would 255
need to pass within 10 m of boresight before their SIR values would exceed the detection 256
threshold. This suggests that the ripple in the near field radiation pattern evident in Fig. 3 and 257
Fig. 4, would exert a stronger control on the observed particle oscillation characteristics in cases 258
where a low background reflectivity (< -20 dBZ) leads to earlier particle detection. 259
260
Other possible radar controls on the oscillation characteristics could arise from range sidelobe 261
contamination and constructive and destructive interference patterns caused by the superposition 262
of signals received from other nearby particles. The motivation for the inclusion of particle-to-263
particle interference stems from the nature of the streaks shown in Figs. 10-12. We first note 264
from the spectra shown in Fig. 12 that the main spectral peaks do not align particularly well with 265
those anticipated for first (or second) fundamental mode of naturally occurring drop oscillations 266
at the inferred diameter. Rather, we find better consistency between the inferred 3.3 mm particle 267
sizes with the secondary maxima evident in all the spectra in the 50 to 60 Hz range (Fig. 12). 268
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Errors in the analysis of the drop size caused by their unknown trajectory through the beam may 269
be one culprit. In the case of S2, the spectral peak near 26 Hz would correspond to a drop 270
diameter of 5.5 mm (Fig. 12a). This would have required errors in the corresponding RCS of 271
approximately 14 dBsm at the observed range (see Eq. A2). 272
273
An alternative explanation for the main spectral peaks evident in Fig. 12 may lie in the nature of 274
the signal associated with the constructive or destructive interference patterns associated with 275
two or more closely located particles (ΔR ~ R6 or less). An expansion of Eq. 2.8 of Doviak et al. 276
(1979) for the simplest possible case of two interacting particles leads to a time fluctuating 277
component of the instantaneous echo power P(τs) given by a term of the form 278
1
2 𝐶(𝜏 )𝑐𝑜𝑠 [
4𝜋(𝑣2−𝑣1)
𝜆
𝑚
𝑃𝑅𝐹]. In this expression C represents the composite amplitude, m/PRF 279
represents time, and fb=2(v2-v1)/λ is the frequency of the fluctuation as a function of the 280
differential radial velocities (v2-v1) between the two particles. This is a statement indicating that 281
the differential range phase between the two particles cycles more quickly as the velocity 282
between the two particles increases. 283
284
A look back at Fig. 10 indicates that at least one of the observed streaks (S2) is really comprised 285
of two nearby particles (labeled S2a and S2b). We can further determine from the plot that these 286
two particles are falling with a differential radial velocity of approximately ~0.7 m s-1. The use of 287
the above expression for fb leads to a predicted resonance frequency of 26.4 Hz, a value that is 288
found to be in good agreement with the location of the main spectral peak shown in Fig. 12a. 289
Numerical simulations of the S2 type drop-drop interference patterns provide further support that 290
this type of interaction can have a strong influence on the temporal evolution of closely located 291
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streaks (Fig. 14; see Appendix A for the simulation details). Note the similarity of the simulated 292
periodicity of the along-streak structure with that of the observed S2 couplet shown in Fig. 10. 293
Offline calculations indicate this oscillation frequency is exactly 26.4 Hz in agreement with the 294
predicted result. This agreement arises even though the drops themselves are held at a fixed 295
diameter and are not allowed to oscillate or otherwise interact dynamically in any manner 296
throughout the course of the simulation. 297
298
The above analysis is meant to show some of the fascinating combinations of cloud particle 299
physics and radar attributes that are possibly contributing to the variability in the observed along-300
streak structure presented in this study. Resonance may be invoked in some instances to help 301
explain why some particles exhibit periodic fluctuations in their time series while other nearby, 302
but somewhat more isolated particles (such as S1 and S6) do not. Other particles, such as S5, 303
will likely have a more complex interpretation as they also appear more isolated yet contain 304
well-defined spectral peaks at specific frequencies not readily attributed to resonance effects 305
alone. In such cases, the inclusion of additional processes such as multi-modal oscillations, drop 306
collision rates, sidelobe impacts, or other factors, may have a greater bearing on the final 307
outcome. The structure of streaks, such as S3, represents an interesting hybrid between S2 and 308
S5 in that the oscillations rapidly dampen in time. This damping is perhaps in response to either 309
natural viscous dissipation processes which are known to have similar time-scales for particles of 310
this size (see Eq. 2 of Beard et al. 1983) or as a result of impacts from other nearby particles. In 311
short, the observed complexity can be challenging to fully understand but it appears promising 312
that enough spectral separation may exist in some instances to further help isolate cause and 313
effect with additional study. 314
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315
Additional Case Studies 316
317
The MCR is capable of deriving the structure of layered cloud systems at a level of detail 318
comparable to high resolution Large Eddy Simulations. One previously published example using 319
the MCR includes a study of the gravity wave impacts on the melting level structure of a 320
convectively generated trailing stratiform cloud shield (Schmidt et al. 2017). They noted that 321
gravity wave updrafts observed near the melting level provided a favorable environment 322
conducive to the production of small water drops and pristine needles in a temperature regime 323
(-3 to -8 °C) known to be favorable for secondary ice particle production (Hallet and Mossop 324
1974). This is similar to the results described in Yuter and Houze (2003) and Houser and 325
Bluestein (2011). The gravity wave downdrafts were found to be associated with larger particle 326
production and aggregates. These contributed to the periodic negative velocity anomalies 327
observed to extend downward from the melting level in a series of wave-induced rain shafts. 328
329
The fine resolution and high sensitivity of the MCR also allows this system to operate as a 330
capable cloud radar. Cloud radars have traditionally been associated with shorter wavelength 331
radars, such as the Ka-band ARM Zenith Radar (KAZR), which have a proven track record for 332
documenting the internal cloud velocity and microphysical signatures [Chandra et al., 2015; 333
Kollias et al. 2016). Recent work has also shown promise for using such radars to estimate the 334
precipitation rates through knowledge of the radar attenuation characteristics (Chandra et al., 335
2015). A comparison of the MCR characteristics with that of KAZR is shown in Table 1. The 336
comparison reveals that the MCR wideband waveform has a higher sensitivity and a comparable 337
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beamwidth to KAZR along with a significant increase in peak power and range resolution. This 338
sensitivity was demonstrated in a study of a mixed-phase altocumulus cloud layer examined by 339
Schmidt et al. (2014). The MCR was able to resolve fine-scale circulations in the altocumulus 340
associated with cloud top entrainment, deeper penetrating updrafts and downdrafts, and subcloud 341
eddy structures associated with descending virga shafts. This sensitivity is also evident in Fig. 13 342
as well as through the detection of clear air signals such as apparent in Fig. 2 near an elevation of 343
4.5 km. These signals near such a high altitude of 4 km are likely not due to insects but rather 344
Bragg scatter from refractive index fluctuations caused by turbulent mixing in a layer at that 345
level of the atmosphere. 346
347
A more recent use of the MCR as a cloud radar is shown in our final example of the higher 348
resolution wideband waveform data obtained for the shallow stratus cloud depicted in Fig. 15a. 349
Broad weak echo regions are evident within the primary updrafts (Fig. 15b,c). There is evidence 350
of very thin layers of enhanced reflectivity (< 10 m thick) that ring the tops and peripheral 351
regions of these rising plumes (labeled ER). These structures are suggestive of preferential 352
increases in either the drop concentration or particle sizes in these regions. Very narrow and 353
vertically coherent channels of weaker reflectivity also extend downward from cloud top and 354
appear to be associated with the cloud-top entrainment process (labeled EC). Very narrow 355
filaments of higher reflectivity tend to form along the periphery and base of these features and 356
near the base of the virga shafts extending below cloud base. A similar feature is found between 357
the U2 and U3 updrafts. Similar features were noted to arise in the study of thin altocumulus 358
cloud layers presented by Heymsfield et al. (1991) and Schmidt et al. (2014). 359
360
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Summary and Future Work 361
362
Highlights from a series of experiments using the MCR have demonstrated this radar serves as a 363
highly capable cloud and precipitation radar. The radar has a high peak power, narrow 364
beamwidth, and extremely small radar resolution volumes that help provide a detailed look at the 365
interior cloud structure at a resolution that may be of interest in many basic research and model 366
validation applications. It has also been shown that it is now possible to observe individual cloud 367
hydrometeors in real cloud systems using a 500 MHz LFM bandwidth waveform. The individual 368
particles generated unique, and at times complex, radar signatures referred to as streaks which 369
provide clues into the underlying cloud hydrometeor structure and behavior. These structures are 370
being analyzed in terms of radar and physically based processes such as multi-drop radar 371
resonance, sidelobe contamination, the onset and viscous decay of diameter-dependent single or 372
multi-modal drop oscillations, drop-drop collisions, and other factors. Future work is required to 373
determine the prevalence of drop couplets such as S2 and to ascertain whether their origins can 374
be tied to specific processes such as the break-up of larger drops. Future field studies will be 375
conducted to obtain additional high-resolution observations of clouds and hydrometeor-induced 376
streaks. It is hoped such observations may help motivate new radar designs and/or research 377
applications that can be used to study other phenomena such as the formation and evolution of 378
damaging hail stones. Possible future collaboration efforts involving dual-polarization cloud 379
radars could be run in a coordinated fashion to further document the radar inferred cloud 380
microphysical structure measurements from multiple points of view. The use of co-located Ka-381
band radars, may be of particular interest to attenuation-based precipitation estimates or other 382
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studies if the MCR can help determine the properties of the individual particles in nearly the 383
same resolution volumes. 384
385
We anticipate that the interaction of two or more drops oscillating at their natural diameter-386
dependent frequencies will provide an even wider variety of responses than those modeled or 387
observed here. Idealized radar-based wind tunnel studies could also be conducted with two or 388
more drops to see if the drop-drop interference signatures reported here could be replicated in a 389
more controlled environment. More realistic numerical solutions could also certainly be designed 390
that include a wider range of differential velocity groupings and additional physical processes. 391
The MCR’s dual-polarization capability which can be used to study drop canting angles, drop 392
aspect ratios, and tumbling ice particles has also yet to be fully exploited. 393
394
Acknowledgements 395
396
This research was supported under grants N0017818WX00186 from the Naval Surface Warfare 397
Center Dahlgren Division. The Authors benefitted greatly from the suggestions and insight of 398
two anonymous Reviewers and the review of Dr. Paul Smith, South Dakota School of Mines. 399
The Authors also benefitted with discussion with Dr. Viswanathan Bringi, Colorado State 400
University; Dr. Jeffery Keeler, NCAR; and Dr. Kevin Knupp, University of Alabama, 401
Huntsville. We also would like to acknowledge the support received from the Cape Canaveral 402
Air Force Weather Station Facility site manager (Dave Chapman), the NASA Space Shuttle 403
Program Manager (Dr. William Parsons), the NASA Debris Radar Project Manager (Anthony 404
Griffith), and personnel at the Naval Ordnance Test Unit (NOTU) for their logistical support, and 405
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air traffic support provided by Mr. Hank Tracy and local air traffic controllers in the Titusville, 406
FL region working within the Federal Aviation Administration. Jamie VanderHeiden of 407
NSWCDD is acknowledged for her help in the experimental planning. Dr. Stephen Schindler of 408
NASA helped secure radiation permission for the ground-based instrumentation. Satellite 409
support for the field programs were provided by Mr. Kim Richardson of the Marine Meteorology 410
Division of the Naval Research Laboratory. Ed Garcia, Nen Nguyen, Daniel Margulieux, Jim 411
Niger, Peter Jones, Joe Ellis, and Fernard Purnell of L3 Interstate Electronics Corporation, 412
Anaheim, CA, provided critical support with the balloon releases, radar data processing, and 413
aircraft tracking algorithms. The Authors are also indebted to the dedicated MCR radar operators 414
Ricky Littleton, David Botterbausch, and James Erbaugh. A special thanks to Dr. David Lando 415
(retired NSWCDD) for his vision, persistence, and patience. And finally, this work would not be 416
possible without the pioneering studies and MCR technical development and direction provided 417
early on by Dr. Julius Goldhirsh (The Johns Hopkins University Applied Physics Laboratory) 418
and Dr. Ed Fletcher (Radar Technology Specialist, Anaheim, CA) who are now both deceased. 419
420
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Appendix A 421
422
Streak Analysis: 423
Factors governing the raindrop size estimates for the MCR were described by Schmidt et al. 424
(2012) and are summarized in Fig. 6 of that study. Individual particle size estimates are derived 425
from the mean peak RCS values (taken near the apex of parabolic plots shown in Fig. 11), the 426
particle slope, or through the use of well-known diameter-dependent factors such as the terminal 427
velocity and particle oscillation frequency (Rayleigh 1879; Gunn 1949; Beard 1976; Pruppacher 428
and Klett, 1978; pgs 315-322; Szakáll et al. 2010). Reflectivity based estimates of the particle 429
diameter (D) take the form D = (R2V1Z)1/6 where R [km] is the range to the target, V1 [m3 km-2] 430
is the range normalized radar pulse volume (V1 = 3.4328), and Z [mm6 m-3] is the along-streak 431
radar reflectivity factor (Z = 10dBZ/10). It is assumed (where applicable) that the background 432
reflectivity does not significantly alter the derived diameter estimates and that the application of 433
the Rayleigh approximation provides reasonable size estimates. The pre-multiplication of Z by 434
the resolution volume (R2V1) in the equation for the particle diameter [D = (R2V1Z)1/6 ] is 435
equivalent to converting reflectivity (which is related to a R2 dependence in the distributed target 436
form of the radar equation) to the sixth power of the diameter of a single-particle 437
(whose received power dependence goes as R4 in the single-particle version of the radar 438
equation). This follows from the Rayleigh approximation used in the weather radar equation (see 439
Doviak et al (1979), Eqs. 2.20 and 2.21). The streak observations shown in this study happen to 440
occur in the near field of the radar (as was first suggested to us by Dr. Paul Smith, South Dakota 441
School of Mines; personal communication). This can lead to a negative reflectivity bias of ~0.71 442
dB for the MCR at a range of 2 km and an under-estimate in the calculated diameter of 443
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approximately 0.1 mm for the observed peak particle RCS values evident in Fig.11. Field 444
measurements will be made in 2019 in an effort to validate the numerical simulations shown in 445
Fig. 3 and Fig. 4 of this study to further quantify the near-field structure of the MCR. We also 446
caution that the various estimates used in this study may not always agree as errors can be 447
expected to arise from a variety of other factors such as the presence of updrafts or downdrafts, 448
the off boresight placement of the streak, the contribution of two or more large particles to the 449
observed reflectivity. Use was made of the regime 2 and regime 3 relationships of Beard (1976) 450
as well as the streak slopes and Doppler analysis to estimate the particle sizes. The lateral motion 451
can be deduced knowing the temporal length of the streak, the range to the target, and knowledge 452
of where the particle crosses of the beam provided a monopulse analysis is conducted. 453
454
Idealized Drop-Drop Simulations: 455
The drop simulations were written in MATLAB for the complex return (V) from two drops at a 456
time (t) and matched filtered range (R) as: 457
458
𝑉(𝑡, 𝑅) = [𝐴(1, 𝑡, 𝑅) + 𝐴(2, 𝑡, 𝑅]𝑒−𝑖𝜃(𝑘0,𝑡) Eq. 1A 459
460
where 461
462
𝐴(𝑘, 𝑡, 𝑅) = 𝐴(𝑘, 𝑡)𝑃[𝑅 − 𝑅(𝑘, 𝑡)]𝑒−𝑖𝜃(𝑘,𝑡) is the complex return for drop k, 𝜃(𝑘, 𝑡) =
−4𝜋𝑅(𝑘,𝑡)
𝜆 463
is the range phase for drop k, 𝜃(𝑘0, 𝑡) =
−4𝜋𝑅(𝑘0,𝑡)
𝜆 is the motion compensation phase for 464
dealiasing the frequencies, 𝑅(𝑘, 𝑡) = 𝑅0(𝑘) − 𝑣𝑘(𝑘)(𝑡 − 𝑡0) is the range from the reference 465
value (R0) and initial time (t0) due to the terminal velocity of the particle (vk), λ is the radar 466
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wavelength (0.053 m), and P[R] is the matched filter output pulse shape using an assumed 467
normal pulse shape fitted to the 6 dB range width of the actual MCR pulse shape (𝑝𝑘 = 𝑒−0.5𝑦2
468
where 𝑦2 =
𝑅𝐺−𝑅(𝑘)
𝜎𝑅
with RG representing the range axis with a gate spacing of 9.1 cm and σR = 469
0.2293 m representing the Gaussian pulse shape approximation to the response antenna 470
weighting as the particle traverses the beam). This approximation only qualitatively accounts for 471
the beam shape in the near field which is shown in Fig. 4 to have imposed ripples in the Fresnel 472
region which we do not attempt to simulate. The plotted time-height data in Fig. 14 are given by 473
10𝑙𝑜𝑔10(|𝑉(𝑡, 𝑅)|2). The motion compensation phase θ(k0,t) is selected from one of the two 474
specified terminal velocities for each particle. We do not attempt to model the hydrodynamic 475
interactions between the drops, the internal drop oscillations, or the viscous damping. 476
477
Near- and Far-Field Region Modeling: 478
479
The MCR’s radiation pattern in the Fresnel region was obtained numerically using the method of 480
spherical expansion provided by GRASP Software (TICRA, Copenhagen, Denmark, 481
www.ticra.com). GRASP is the industry standard for analyses of electromagnetic radiation 482
emitted from large reflector antennas (Jorgensen et al 2018; Cappellini and Salghetti-Drioli 2016). 483
A representative down-range of 1940 m discerned from Fig. 10 was selected for the Fresnel 484
region simulations using a 0.01 m grid spacing over a 15 m by 15 m mesh. An arbitrary down-485
range of 10,000 m was selected for the Far-field region simulations using a 0.5 m grid spacing 486
over a 1250 m by 1250 m mesh. These numerical simulations account for the size of the MCR’s 487
dish, transmitted power, wavelength, and right-hand-circular emitted polarization, as well as the 488
size, location and alignment of the feed horn, sub-reflector and struts relative to the dish, 489
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obtained from MCR design documents. The Fresnel (far-field) simulation results were projected 490
onto a cross-range plane located at a down-range distance of 1940 m (10,000 m), perpendicular 491
to the boresight direction. 492
493
The inverses of Eqs. (10) and (16) from Sekelsky (2002) were used to derive estimates of the 494
boresight gain and reflectivity factor corrections in the Fresnel region, using the power density 495
function derived from the near field simulation at 1940 m down-range and the far-field 496
simulations at 10,000 m down-range. The derived corrections were 0.71 dB and 0.66 dBZ for 497
the gain and reflectivity factor corrections, respectively, which are smaller than those predicted 498
by Eqs. (17) and (20) of Sekelsky (2002), likely due to the unique structural and radiation 499
characteristics of the MCR (e.g., -12 dB sub-reflector illumination, and dish-edge taper level of -500
20 dB). Regarding the calculations of signal-to-interference ratio (SIR) of Fig. 13, Eq. (2.2) of 501
Doviak et al (1979), and Eqn. 1A of Schmidt et al (2012) were utilized along with the 2-way, 502
normalized radiation function ( 𝑓4(𝜃, 𝜙)) derived from the near field simulation at 1940 m 503
down-range to derive the following expression: 504
505
𝑆𝐼𝑅 =
𝜋5|𝐾𝑝2|
2
𝐷6 𝐿𝐺 𝑓4(𝜃,𝜙)
𝜆4𝑅4(𝑍𝑁𝑅+1) Eq. 2A 506
507
where D is the particle diameter, λ is the radar wavelength, LG is the MCR loop gain expressed 508
as a power ratio of the signal power to noise power and has a value of 1027 m2 (or 270 dB), Kp is 509
the dielectric constant of the particle, R is the down-range to the particle, and ZNR is the 510
background (ZNR) signal-to-noise power ratio given by ZNR = dBZbk -20log10(R) + 111.21 511
where dBZbk is the background reflectivity value (dBZ). Owing to the small angular spread in 512
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the cross-range compared to R, the products of R with both the transverse and elevation angles, 513
𝜙 and 𝜃, are equated to the Cartesian x and y coordinates, respectively, which locate the points 514
in the cross-range plane of the simulations. Since the antenna pattern shown in Fig. 3a is 515
circularly symmetric, and only varies by ~0.1 dB with no significant change in shape (not 516
shown) over the ~10 m range of altitude spanned by the falling raindrop streaks shown in Fig. 517
10, for simplicity, it is assumed that the 3mm raindrop traverses the MCR beam while travelling 518
along the x-axis of Fig. 3a between -15 m < x < 15 m. 519
520
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679
Parameter MCR UND
North Pol
CSU
CHILL
NCAR S-
Pol WSR-88D KAZR
Frequency (GHz) 5.4 – 5.9 5.6 2.725 2.7 – 2.9 2.7-3.0 34.86
Transmit Polarization Right
Circular Linear H, V
Linear H,
V, Slant
45/135,
Right and
Left
Circular
Linear H, V Linear H, V Linear H
Receive Polarization
Right and
Left
Circular
Linear H, V
Linear H,
V, Slant
45/135,
Right and
Left
Circular
Linear H, V Linear H, V Co-/Cross-
Polar
Antenna Dish Diameter
(m) 15.24 3.66 8.5 8.5 8.5 2 to 3
Beamwidth (degrees) 0.22 0.99 1.1 0.91 0.925 at 2850
MHz 0.31 to 0.19
Peak Power (MW) 3 0.25 0.8 to 1.0 1.0 0.7 0.002
Maximum Pulse Rate
(Hz) 320 1000 1250 1300 1304 10000
Pulse Width (s) 12.5
(LFM) 0.6 to 2.0 0.2 to 1.6
(Gaussian)
0.3 to 1.4
(Tapered) 1.57 to 4.71 0.03 to 12
(NLFM)
Maximum/Minimum
Range Resolution (m) 0.543/34.0 90/300 30/150 38/1000 250/1000 30
Sensitivity at 5 Km
Range [Z (dBZ)]
-57 (NB)
-38(WB)
-28 -24 -29 -28 to -37 -31
Sensitivity at 150 km
Range [Z (dBz)]
-26 (NB)
-8 (WB)
2 6 1 2 to -7
-1 (150 km
range not
attainable)
-21 (at
15km)
Typical Scan Range
Interval (km)
75 (NB)
0.375 (WB)
150 150 150
300
(Doppler)
460 (dBZ,
dual-Pol)
15
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680
Table 1. The Table provides characteristics of the MCR and a selection of standard weather 681
research radars including the UND North Pol, the CSU-CHILL, the NCAR S-Pol, WSR-88D, 682
KAZR Ka-band (Kollias et al. 2016; Chandra et al. 2015) Doppler radars. The UND North Pol is 683
a Weather Surveillance Radar designed in 1974 (WSR-74C) that has since been upgraded to a 684
dual polarization system. See text for more details (Adapted from Rinehart (2004) with updates 685
from the CHILL and S-Pol Radar websites, and personal communication with UND). 686
687
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Instrument Manufacturer Parameter Resolution Frequency/
Wavelength
CL51 Ceilometer Vaisala Backscatter 10 m Gate Spacing @ 1 min 910 nm
Micro Pulse Lidar Sigma Space Backscatter 5/15/30/75 m Gate Spacing
@ 1 min
532 nm
Micro Rain Radar METEK dBZ, Ur, PSD, Nt, LWC 30 Range Gates (30-6000 m) @
10-3600 s
24 GHz
MP3000A Radiometrics T, Qd, LWC 50-500 m Gate Spacing @ 2 min V & K-band
Parsivel2 Disdrometer OTT Nt, VT, dBZ, Visibility 20 Bins: 200 µm-8 mm (liquid)
200 µm-25 mm (solid)
650 nm
All-Sky Camera Prede Cloud Images 5 Megapixel Image @ 1 min Visible
Snow White Meteolabor T, Td, P, U, V 0.5 to 2 s Response Times
Doppler Lidar Halo Photonics Ur, Back Scatter 18 m @ 10 Hz 1.5 µm
Sonic Anemometer Gill U, V, W, T 20 Hz
Li-7500DS LiCor H2O, CO2 20 Hz
FM120 Droplet Measurement
Technologies
PSD, Nt 30 Channels (2-50 um)
AQT420 Vaisala Gas Concentration (NO2, SO2, CO,
O3) Particle Matter (PM2.5, PM10)
60 s Averaging
WXT520 Vaisala T, P, RH, Precipitation, SPD, DIR 4 Hz
Ka-Band Doppler Radar ProSensing dBZ, Ur 30, 75, 100 or 150 m 35.4 GHz
*Liquid Water Content Probe King LWC 1 Hz
*Two-Dimensional Optical
Array Imaging Probe
Particle Measuring
Systems
Particle Images, PSD, Nt 32 Diodes of 25 um Each,
Asynchronous Data
*Water Content Probe Nevzorov Total Water Content, LWC 25 Hz
*TT102 Rosemount T 1 Hz (2 s Response Times
*FSSP Particle Measuring
Systems
PSD, Nt 30 Channels (2 – 47 µm), 1 Hz
Data
*239 Pressure Probe Setra ±0.05% & ±0.14% Full Scale 20 ms Response Time
*Td Probe Model 137 EdgeTech Td 25 Hz Data (1.5 °C s-1
Response Time)
*TDL Maycomm Research Co. Qv 1.6 Hz
*POSAV 310 and 5 Port Gust
Probe
Applanix U,V,W 25 Hz
*2D-S Stratton Park Engineering
Company, Inc.
Particle Images, PSD, Nt 128 Diodes of 10 µm Each,
Asynchronous Data
*HVPS3 Stratton Park Engineering
Company, Inc.
Particle Images, PSD, Nt 128 Diodes of 150 µm each,
Asynchronous Data
*CDP Droplet Measurement
Technologies
PSD, Nt 30 Channels (2-50 µm), 10 Hz,
Particle-by-Particle Data
688
Table 2: A list of the primary surface-based and airborne (denoted by asterisk) instrumentation 689
used during the 2008-2015 field campaigns and/or planned for 2019. The research aircraft have 690
included the North Dakota Cessna Citation II jet aircraft and the dual prop Cessna Cheyenne 691
Accepted for publication in Bulletin of the American Meteorological ociety. DOI S 10.1175/BAMS-D-18-0130.1.
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aircraft operated by Weather Modification International. Aircraft measurements were acquired 692
using a Science Engineering Associates model M300 data acquisition system and processed 693
using the Airborne Data Processing and Analysis Software Package (Delene 2011). The symbols 694
have the following meanings: pressure (P), temperature (T), dewpoint temperature (Td), liquid 695
water content (LWC), relative humidity (RH), water vapor density (Qd), water vapor mixing ratio 696
(Qv), east-west, north-south, and vertical wind components (U,V,W), wind speed (SPD), wind 697
direction (DIR), particle concentration (Nt), particle size distribution (PSD), High Volume 698
Particle Spectrometer Version 3 (HVPS3), Two-Dimensional Stereographic Optical Array Probe 699
(2D-S), Position and Orientation System for Airborne Vehicles Model 310 (POSAV 310), 700
Tunable Diode Laser Hygrometer model AC19-400 (TDL), Forward Scattering Spectrometer 701
Probe (FSSP), microwave radiometer (MP3000A), Cloud Droplet Probe (CDP), Fog Monitor 702
Model 120 (FM120), reflectivity (dBZ), Doppler radial wind component (Ur), terminal velocity 703
(VT), and Total Temperature Probe Model 102 De-iced (TT102). The four field experiments 704
were conducted during the following periods: 7-18 July 2008, 13-24 July 2009, 16-27 August 705
2010, 27 July to 9 August 2015. 706
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707
708
709
Fig 1: The U.S. Navy Mid-Course Doppler Radar located near Titusville, FL as pictured during a 710
study of an altocumulus layer on 8 August 2015. 711
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712
Fig. 2: Experimental design for the CAPE Weather Experiments held in the Titusville, FL 713
region. The shaded backdrop is a time-height image of the MCR-derived cirrus and mammatus 714
cloud reflectivity obtained between 22:16 and 22:54 UTC 8 August 2015. The bold red and 715
green lines represent the temperature and dewpoint temperature data derived from a balloon 716
launch at 1749 UTC 8 August 2015 (scaled in arbitrary units). The primary surface instruments 717
include the Sigma Space micropulse lidar (black rectangle) and the MCR dual polarization C-718
band Doppler radar. The pictured aircraft is the instrumented University of North Dakota’s 719
Cessna Citation II aircraft. The MCR is depicted as tracking the research aircraft in real-time 720
while the lidar is used to guide the placement of the aircraft and the short MCR wideband range 721
window. 722
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723
724
Fig. 3: The simulated MCR near-field calculated at a range of 1.94 km from the radar showing 725
the (a) power density (dB) and (b) phase (degrees) for a transmitted pulse having a right hand 726
circular polarization. The contour interval in (a) is 5 dB and 30 degrees in (b). The dashed white 727
line in each plot shows the location of the cross-section plots shown in Fig. 4. 728
729
Accepted for publication in Bulletin of the American Meteorological ociety. DOI S 10.1175/BAMS-D-18-0130.1.
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730
731
Fig. 4: The MCR simulated cross-beam antenna patterns showing: (a) the power density (dB), 732
and (b) the phase (degrees). The black curve in (a) shows the power density at 1.94 km range 733
whereas the red curve in (a) shows the power density at 10 km range, normalized in the across 734
range direction by the range-angular factor of 1.94/10. The black dashed lines in (a) and (b) are 735
the 3 dB beamwidth, and the equivalent phase angle level corresponding to the 3dB beamwidth 736
level measured across boresight in (a), respectively. 737
738
739
Accepted for publication in Bulletin of the American Meteorological ociety. DOI S 10.1175/BAMS-D-18-0130.1.
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740
741
742
743
Fig 5: Multi-component analysis of the aircraft pass through the 1 August 2015 anvil system 744
pictured in (a) as the aircraft was tracked by the MCR: (b) range-time and along-track MCR 745
narrowband reflectivity [dBZ], (c) in situ measurements of temperature (°C), pressure (hPa), 746
total water (black) and liquid water content (blue) [g m-3], and (d) 2D-S images from the 2D-S 747
showing ice crystal chain aggregates (circled in red). The vertical width of each panel in (d) 748
represents 1280 µm and each panel represents less than one second of elapsed time. The particle 749
images were acquired during the anvil penetration when the aircraft was at a temperature of 750
~-43.5 °C. The bold letter ‘o’ in (b) denotes the location of the crystal images shown in (d). 751
Accepted for publication in Bulletin of the American Meteorological ociety. DOI S 10.1175/BAMS-D-18-0130.1.
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752
753
Fig. 6: The time-height cross-section of the MCR narrowband reflectivity recorded between 754
2145 and 2215 UTC 24 July 2009 (shaded) at a time when streaks were being observed with the 755
MCR wideband waveform. The white boxes labeled B1 and B2 denote the location of the 756
wideband reflectivity shown in Fig. 7 and Fig. 8, respectively. The precipitation streamer labeled 757
R1 denotes the primary rain shaft depicted with the same labeling in Fig. 8. The length-scale is 758
based on an estimate of the reflectivity cell movement of 5 m s-1 as observed with the Melbourne 759
WSR-88D Doppler radar during the time of interest. 760
761
Accepted for publication in Bulletin of the American Meteorological ociety. DOI S 10.1175/BAMS-D-18-0130.1.
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762
763
Fig. 7: Time-height plot of the MCR wideband reflectivity structure (shaded) for the portion of 764
the storm associated with the fast rising turret discussed in the text (encapsulated in the box 765
labeled B1 of Fig. 6). The discovery occurred 10 minutes prior to shutting down the radar for the 766
2009 field campaign as the last scan of the day was being executed. 767
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768
769
Fig. 8: As in Fig. 7 except the data are taken at the time corresponding to the box labeled B2 in 770
Fig. 6. The linear reflectivity features in this time-height plot represent individual hydrometeors 771
and are denoted as radar reflectivity “streaks”. 772
773
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774
775
776
Fig. 9: Rain shaft and drop structure derived from the MCR wideband waveform as the storm 777
system pictured in (a) approached the radar on 30 July 2015. The wideband derived reflectivity 778
of the rain shaft (b) and of the individual raindrops (c) are taken at different times during the 779
storm passage. The vertical scale and elapsed time shown in (b) and (c) are ~320 m and 180 s, 780
respectively. The images are inverted so that time increases from right to left. 781
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782
Fig. 10: High-resolution time-height plots of the MCR wideband radar cross section (RCS) for a 783
3.4 second time window taken during the 30 July 2015 storm system. The data reveal the 784
detailed structure of the individual cloud hydrometeors passing through the vertically orientated 785
radar beam. The data represent the pulse-to-pulse structure and is presented without any temporal 786
or spatial averaging. The “streaks” labeled S1, S2, S2a, S2b, S3, S4, S5, and S6 are discussed in 787
the text. The bold white arrows labeled S2a and S2b highlight the position of the two streaks 788
comprising the S2 streak. 789
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790
791
Fig 11: The pulse-to-pulse RCS values (dBsm) obtained along the primary axis of the streaks: (a) 792
S2a, (b) S3, and (c) S5 shown previously in Fig. 10. The bold dashed line in each panel 793
represents a fourth-order polynomial fit to the data. The maximum drop diameter taken at the 794
apex of the fitted dashed curve is denoted in each panel. 795
796
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797
798
799
Fig. 12: A power spectra analysis of the amplitude fluctuations for the streaks labeled: (a) S2b, 800
(b) S3, and (c) S5 shown previously in Fig. 10 and Fig. 11. The shading in each plot is the 801
spectral power [dBsm Hz-1] derived from a sequence of 128 pulse subsets (ni = ns:ns+128) taken 802
from the original streak time series. The starting pulse number (ns) for each successive subset 803
was incremented by a value of one from that used in the previous subset. The red solid curve 804
represents the mean value of the power at each frequency derived over all subsamples. The plot 805
was normalized and then scaled by the total number of subsamples in each panel so each mean 806
spectral just covers the entire plot. The bold dashed line white line represents the theoretical drop 807
oscillation frequency (fd) as a function of diameter (right ordinate) derived from Eq. 2 of Szakáll 808
et al. (2010). The frequency of the main spectral peaks is high-lighted by the white text. 809
810
Accepted for publication in Bulletin of the American Meteorological ociety. DOI S 10.1175/BAMS-D-18-0130.1.
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811
Fig. 13: The minimum detectable particle diameter (mm) for a water drop at the specified ranges 812
of 2.0 km (solid), 4.5 km (dashed), and 10 km (dot-dashed) derived from Eq. A2. The solid black 813
dots labeled F7, F8, F9, F10, and R1 represent mean conditions for the streaks shown Fig.7, Fig. 814
8, Fig.9, Fig.10, and within the precipitation streamer labeled R1 in Fig. 8, respectively. The 815
value of the Signal to Interference Ratio (SIR) used in Eq. A2 was set to 3 dB. 816
817
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818
819
820
Fig. 14: Idealized simulations of the RCS [dBsm] for the case of two drops with specified fixed 821
diameters representing the S2a (D2) and S2b (D1) drop interaction. The differential velocity is 822
set to 0.7 m s-1 as observed. The drops are initially separated by a range of 1.4 m with specified 823
fall speeds of either 5.5 and 4.8 m s-1 for the D1 and D2 particles, respectively. 824
825
Accepted for publication in Bulletin of the American Meteorological ociety. DOI S 10.1175/BAMS-D-18-0130.1.
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826
827
828
Fig. 15: Data from the low-level stratus case of 08 August 2015 case day showing: (a) the all-sky 829
camera imagery of the cloud layer at 1347 UTC, (b) the MCR-derived narrowband reflectivity 830
[dBZ], and (c) the MCR-derived total vertical velocity [ms-1]. The labels U1, U2, and U3 in (b) 831
and (c) denote regions of updrafts discussed in the text. The labeled arrows denote very thin 832
enhancements in the reflectivity at the top and periphery of the U2 (and other) updrafts (labeled 833
ER) and a narrow reflectivity minimum indicative of cloud top entrainment (labeled as EC). The 834
horizontal scale shown is based on an advective speed of ~10 m s-1. The reflectivity and velocity 835
values were derived using 64 temporally consecutive pulse samples. 836
Accepted for publication in Bulletin of the American Meteorological ociety. DOI S 10.1175/BAMS-D-18-0130.1.