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LABLE: a multi-institutional, student-led, atmospheric boundary layer experiment.

This paper presents an overview of the Lower Atmospheric Boundary Layer Experiment (LABLE), which included two measurement campaigns conducted at the Atmospheric Radiation Measurement (ARM) Program Southern Great Plains site in Oklahoma during 2012 and 2013. LABLE was conducted as a collaborative effort between the University of Oklahoma (OU), the National Severe Storms Laboratory, Lawrence Livermore National Laboratory (LLNL), and the ARM program. LABLE can be considered unique in that it was designed as a multiphase, low-cost, multiagency collaboration. Graduate students served as principal investigators and took the lead in designing and conducting experiments aimed at examining boundary layer processes.

The main objective of LABLE was to study turbulent phenomena in the lowest 2 km of the atmosphere over heterogeneous terrain using a variety of novel atmospheric profiling techniques. Several instruments from OU and LLNL were deployed to augment the suite of in situ and remote sensing instruments at the ARM site. The complementary nature of the deployed instruments with respect to resolution and height coverage provides a near-complete picture of the dynamic and thermodynamic structure of the atmospheric boundary layer. This paper provides an overview of the experiment including 1) instruments deployed, 2) sampling strategies, 3) parameters observed, and 4) student involvement. To illustrate these components, the presented results focus on one particular aspect of LABLE: namely, the study of the nocturnal boundary layer and the formation and structure of nocturnal low-level jets. During LABLE, low-level jets were frequently observed and they often interacted with mesoscale atmospheric disturbances such as frontal passages.


The atmospheric boundary layer (ABL) is the lowest level of the troposphere that is directly influenced by interactions with the surface of Earth. Over land, it has a marked diurnal cycle due to the diurnal heating and cooling of the land surface (Stull 1988). Accurate predictions of ABL properties and processes are very important for a variety of applications including weather forecasting, air quality studies, public health, and wind energy (Fernando and Weil 2010; Banta et al. 2013; Holtslag et al. 2013; Hu et al. 2013a,b,c; Klein et al. 2014). During daytime, a well-mixed convective boundary layer (CBL) develops, which can be several kilometers deep. Within the CBL, turbulence covers a wide range of scales extending from kilometers for the large energy-containing eddies down to millimeters for the smallest dissipative eddies (Wyngaard 2010). During the early evening transition (EET), the ABL structure changes quickly and becomes more complex than during the daytime (Acevedo and Fitzjarrald 2001). As the surface cools because of radiative heat losses and lack of solar heating, turbulence decays rapidly, and a stable thermal stratification develops in a layer close to the ground: the stable boundary layer (SBL) is being formed. Flow characteristics similar to the CBL from the previous day often persist in the region between the SBL and the capping inversion, which is why this layer is called the residual layer. The multilayer structure of the nocturnal boundary layer (NBL) poses challenges for both the observation and modeling communities (Fernando and Weil 2010; Baklanov et al. 2011; Holtslag et al. 2013; Hu et al. 2013a), and the factors controlling the interactions between the SBL and residual layer are currently not well understood. Under many circumstances, the turbulent exchange between the residual layer and the SBL is limited, and the residual layer becomes decoupled from the SBL (Mahrt 1999, 2014). This situation may be altered by the presence of a nocturnal low-level jet (LLJ) or mesoscale disturbances.

The LLJ is an ABL phenomenon that is commonly observed over the Great Plains of the United States (e.g., Blackadar 1957; Bonner 1968; Parish et al. 1988; Mitchell et al. 1995; Stensrud 1996; Zhong et al. 1996; Whiteman et al. 1997; Banta et al. 2002; Song et al. 2005; Walters et al. 2008) and at other locations worldwide (e.g., Beyrich et al. 1997; Baas et al. 2009). The jet typically begins to develop around sunset, under dry cloud-free conditions conducive to strong radiative cooling, reaching its peak intensity toward the end of the night, and then decaying after dawn with the onset of daytime convective mixing. The wind maximum typically occurs at levels less than 1 km above ground and frequently happens within the lowest 500 m. The peak LLJ wind speeds are often supergeostrophic by approximately 70% but can exceed the geostrophic values by several hundred percent in strong cases (e.g., Hoecker 1963; Bonner 1968; Brook 1985). The vertical wind distribution in an LLJ typically has a distinctive shape characterized by a pronounced wind maximum, often referred to as the LLJ nose. Despite the presence of strong shear associated with these LLJs, turbulent transport below the wind maximum may be inhibited because of the damping effect of stable stratification on turbulence production; however, there are cases where the turbulence levels remain high or the turbulence is intermittent (Banta et al. 2006). Characterizing the complex nature of the NBL structure and turbulence was one of the motivations for LABLE.

To better understand the dynamic and thermodynamic structure of the ABL, high temporal resolution profiles of mean and turbulent quantities of wind, temperature, humidity, and other trace gases throughout the entire ABL depth are needed (NRC 2009, 2010). Recent studies have highlighted the skill of ground-based remote sensing instrumentation in providing reliable observations of wind, temperature, and humidity profiles in the ABL (Wang et al. 2007; Newsom et al. 2008; Banta 2008; Friedrich et al. 2012; Banta et al. 2013; Barthelmie et al. 2014; Turner and Lohnert 2014). However, questions concerning the accuracy of remotely sensed ABL parameters remain, the collected datasets are often limited, and the interactions of ABL processes with synoptic-scale conditions, orography, and land surface characteristics are still not well understood. To provide new insights into spatial and temporal variations of turbulent processes within the ABL, LABLE combined instruments of different operating principles, temporal and spatial resolutions, and sensitivities and assessed their accuracy against in situ observations. The complementary vertical resolution and range of the various instruments provided a near-complete picture of the thermodynamic, dynamic, and turbulence structure of the ABL at spatial and temporal resolutions, which was, to our knowledge, not met in previous studies.

The LABLE experiments had four primary scientific objectives: 1) to compare observations of mean and turbulent motions from Doppler wind lidars and sodars and to characterize their mean accuracy and sensitivity over a range of different environmental conditions (e.g., CBL vs SBL, high- vs low-wind speed conditions), 2) to assess the accuracy and reliability of temperature profiles measured with the Atmospheric Emitted Radiance Interferometer (AERI), 3) to obtain a better understanding of the structure and turbulent processes within the NBL and their interaction with larger-scale weather patterns, and 4) to investigate how turbulent statistics, such as variance and skewness profiles of vertical motions, vary with upwind land surface conditions. Another unique objective of LABLE was to provide experience for graduate students in observational ABL studies covering all aspects from the design of a field campaign to the scientific analysis of the collected datasets. The goal of this paper is to provide an overview of the LABLE campaigns and the types of data collected. The results presented focus on the first three goals mentioned above. Naturally, the LABLE observations can be used for a range of different studies, and ideas for future analyses are discussed in the conclusions and outlook.

LABLE CAMPAIGNS. The two LABLE field campaigns were organized and conducted by the Boundary Layer Integrated Sensing and Simulation (BLISS) group at the National Weather Center (NWC) in Norman, Oklahoma. The BLISS group brings together graduate students, professors, and scientists from the School of Meteorology at the University of Oklahoma (OU) and from NOAA's National Severe Storms Laboratory (NSSL). It facilitates interagency coordination of research and education efforts in boundary layer meteorology, as well as the integration of in situ and remote sensing instrumentation with numerical modeling techniques. The two LABLE campaigns were designed as low-cost experiments that leveraged existing instrumentation and ongoing collaborations with the Department of Energy's Atmospheric Radiation Measurement (ARM) Program (Mather and Voyles 2013) and Lawrence Livermore National Laboratory (LLNL). Weekly meetings of the BLISS group served as a platform for developing the general deployment strategies for the two campaigns. Graduate students served as principal investigators, playing a leading role in the experiment design, the day-to-day operation of the various instruments, and the data acquisition and storage, quality assurance, and scientific analysis of the collected datasets. The experimental design of the LABLE I campaign, which ran from 18 September to 13 November 2012, was more driven by the scientific objectives outlined by senior personnel, although the graduate students were able to provide input and gained useful experience in the deployment and operation of the instruments. During the weekly BLISS meetings, updates were given about the status of the various instruments and data streams, and possible changes to the experimental plan were discussed. Graduate students also developed scripts to integrate different data streams and to create quick-look plots that allowed assessing the data quality in near-real time. For LABLE II, which was from 12 June to 3 July 2013, two Ph.D. students independently developed specific DL deployment and scanning strategies to obtain datasets that are essential for their Ph.D. research. With the experience gained during LABLE I, the students were able to conduct the experiment requiring only minor support from senior personnel.

INSTRUMENTATION AND OBSERVATIONAL STRATEGIES. LABLE was conducted at the ARM Southern Great Plains (SGP) site, located in north-central Oklahoma in rural terrain with primarily pasture and farmland (Fig. 1a). All LABLE instruments were deployed at the SGP central facility (Fig. 1b) near Lamont (36.606[degrees]N, 97.485[degrees]W), which is approximately a 2-h drive north of the main OU campus. The SGP central facility operates a wide range of in situ and remote sensing instrumentation for monitoring of the ABL (Mather and Voyles 2013). Of particular interest for LABLE were the ARM Streamline Doppler lidar (DL), 915-MHz wind profiler, water vapor and aerosol Raman lidar, AERI, rawinsonde releases four times per day, and flux observations made by sonic anemometers and infrared gas analyzers at 4 m above ground level (AGL) at an eddy correlation (ECOR) flux measurement system and at 25 and 60 m AGL on a 60-m tower. During the LABLE I campaign, BLISS deployed three additional wind profiling instruments (2 DLs and a sodar); during LABLE II three DLs were deployed. Details about the siting and specifications of all instruments used for the LABLE I and II studies can be found in Fig. 1 and Table 1; Fig. 2 shows photos of the primary LABLE instruments. Data from the 915-MEIz radar wind profiler have been compared with DL observations, but these comparisons are not included in this paper since we primarily focus on the lowest 2 km of the ABL where the resolution of the DL and sodar are superior to the radar wind profiler. Important aspects of the ARM instrumentation utilized for this study are shortly summarized thereafter, before the DL scanning strategies are described in detail.

Raman Mar and AERI. The ARM SGP Raman lidar is an operational system that was designed to measure water vapor, aerosols, and clouds over the diurnal cycle (Goldsmith et al. 1998). The lidar transmits a pulsed laser beam vertically at 355 nm and measures the backscattered photons from Rayleigh-Mie scattering as well as Raman scattering by water vapor and nitrogen molecules. These measurements are used to derive profiles of water vapor mixing ratio, aerosol backscatter, and the extinction coefficient, as well as other geophysical variables (Turner and Goldsmith 1999; Turner et al. 2002). The system was upgraded in 2004 with new detection electronics (Newsom et al. 2009), greatly improving the signal-to-noise ratio in the various products (Ferrare et al. 2006), and new channels to profile temperature (Newsom et al. 2013). The improved capability allows water vapor turbulence profiles in the CBL to be derived from lidar observations (Wulfmeyer et al. 2010; Turner et al. 2014). The AERI is a passive interferometer that measures downwelling infrared radiance from which ABL profiles of temperature and humidity are retrieved (see discussion of the Atmospheric Emitted Radiance Interferometer in the sidebar).

Eddy correlation flux measurements. The combined sonic and infrared gas analyzer measurements at the ARM ECOR system site and 60-m tower collect time series of all three velocity components (u, v, and w), sonic temperature T (which is a good measure of virtual temperature), water vapor, and C[O.sub.2] densities with a sampling frequency of 10 Hz at 4, 25, and 60 m AGL. Using the eddy covariance approach, 30-min mean estimates of the fluxes of momentum, C[O.sub.2], latent heat, and sensible heat are computed from the raw time series applying several quality assurance techniques (Kaimal and Finnigan 1994; Cook 2011). The 10-Hz sonic anemometer data are first passed through a spike filter to eliminate noisy and erroneous data. Data points that are more than a prescribed number of standard deviations away from the 100-s running mean are set to the value of the running mean and are not used in subsequent calculations of the running mean quantities. Before calculating the fluxes, a 2D coordinate rotation is applied, which forces the mean values of u and w to be zero. Webb Pearmann-Leuning corrections are also applied (Webb et al. 1980; Fischer 2004).

Sodar. During LABLE I, a Metek PCS.2000 sodar owned by OU was operated with an acoustic frequency of 1895 Hz in a Doppler beam-swinging (DBS; Strauch et al. 1984) mode consisting of five beam directions with a zenith angle of 17.8[degrees] for the four off-vertical beams. The system completed a five-beam scan every 15 s, and the Doppler spectra were incoherently integrated over a period of 10 min to improve the signal-to-noise ratio (SNR). The maximum possible sensing height of this system was 500 m, and the typical maximum retrieval height during LABLE was approximately 200 m. The percentage of time the sodar was operational during LABLE I is 99.5% (the only time it was turned off was for repair). The sodar observations used in this paper were cluster-analyzed wind component values, which are a direct output from the Metek PCS.2000 sodar. Radial components from instantaneous spectra with sufficiently high SNRs are sorted into classes of width 0.1 m [s.sup.-1], and cluster identification is performed using a running acceptance window of width 1 m [s.sup.-1] . Averaging the samples within the 1 m [s.sup.-1] window containing the highest overall number of samples identifies the radial velocity. The cluster algorithm for evaluation of instantaneous spectra was performed at the sodar averaging period of 10 min. Only 10-min cluster-analyzed data of the zonal and meridional wind components u and u with an SNR of [greater than or equal to] 3 dB were used for wind speed and direction analysis. The 3-dB threshold was chosen, as it is used internally in the sodar software to filter data for the cluster analysis. At a height of 150 m, the SNR was [greater than or equal to] 3 dB for the following percentages of time: 59.0% (day), 49.3% (night), and 54.1% (all). For a lower height of 100 m, the equivalent [greater than or equal to] 3-dB values are 80.8% (day), 69.2% (night), and 75.0% (all). Here, day and night refer to the time periods 1200-2400 and 0000-1200 UTC, respectively.

Doppler lidars. During LABLE I, there were three DLs operating at the SGP site. The operational ARM Streamline DL and the OU Streamline DL are identical systems (except for the OU instrument having an extended range) that were manufactured by Halo Photonics (Pearson et al. 2009). The vendor Leosphere loaned the third DL, a Leosphere WINDCUBE 200, to NSSL for this experiment. These three commercially available DLs use pulsed 1.5-[micro]m lasers and detect the backscattered energy from aerosol particles in the boundary layer. The percentages of time the Streamline lidars were up and running during LABLE I are 100% for the ARM Streamline and 85.6% for the OU Streamline. Over the entire day and night at a height of 1000 m, the SNR was greater than -21 dB for 89% of the time for the ARM Streamline and 82.5% for the OU Streamline. The corresponding numbers for the ARM (OU) Streamline systems are 88.6% (82.2%) at night (0000-1200 UTC) and 89.4% (82.8%) during the day (1200-2400 UTC).

During LABLE I, the ARM Streamline DL performed a plan position indicator (PPI) scan at a 60[degrees]-elevation angle every 15 min in order to derive horizontal winds using the velocity azimuth display (VAD) technique. These PPI scans used eight azimuthal angles and took approximately 1 min. During the remaining time the ARM Streamline DL collected radial velocities in the zenith direction (i.e., vertical velocities). The OU Streamline DL also performed PPI scans but at both 40[degrees] and 70[degrees] elevations. The lower elevation angle improved the accuracy of the horizontal winds in low-wind speed conditions and at lower altitudes, whereas the higher elevation angle was selected to improve measurements of the high wind speeds. These PPI scan pairs occurred every 30 min and used 72 azimuthal angles during most of LABLE I. Between the PPI scans, the OU Streamline DL collected vertical velocity data. The Leosphere WINDCUBE 200, which was located directly adjacent to the Raman lidar, only collected vertical velocities to obtain continuous datasets for the analysis of turbulence properties and water vapor fluxes in the ABL.

During LABLE II, we rented a Galion DL from SGURR energy and deployed it along with the OU Streamline DL and a Leosphere WINDCUBE v2, which is owned by LLNL. The Galion DL is nearly identical to the Streamline DLs (Table 1). We focused on testing different scanning strategies with the Galion and two Streamline systems to obtain high-resolution datasets that can provide accurate turbulence statistics for evaluating data collected with commercially available profiling lidars such as the Leosphere WINDCUBE v2, which employs a DBS technique to measure the three-dimensional wind vector. In each WINDCUBE DBS scan, the lidar beam is pointed toward the four cardinal directions at an elevation angle of 62[degrees] and then pointed vertically. It takes just under 1 s to collect measurements in each beam direction, such that a full DBS scan is completed approximately every 4 s. However, the WINDCUBE v2 velocity algorithm calculates the m, u, and w components every second using the four preceding radial velocity measurements (Cariou 2011).

Doppler Mar scanning strategies and signal processing. One of the goals of LABLE II was to evaluate different lidar scanning techniques for measuring turbulence. When the DBS technique is used to measure turbulence, three major problems cause the lidar to measure different turbulence values than would a sonic anemometer (e.g., Sathe et al. 2011; Sathe and Mann 2012). The first problem is inherent in all remote sensing technology and involves averaging within the probe volume. In the LABLE experiments, lidar range gates were between 18 and 30 m; thus, turbulence scales smaller than these lengths could not be measured accurately. Next, in order to solve the DBS equations, it must be assumed that the velocity is uniform throughout the scanning circle formed by the various beam positions. For low heights and uniform terrain, this assumption is likely valid at times but becomes invalid for higher measurement heights and complex terrain. Finally, the use of only four off-zenith beams to calculate three-dimensional turbulence introduces systematic errors. Sathe and Mann (2012) show that the calculated variance values of u, v, and w are contaminated by the cross components of the Reynolds stress tensor; that is, the variance of the v component has contributions from not just the v component of the wind but the u and w components as well.

While the scanning strategy of the WINDCUBE v2 lidar could not be changed to mitigate these issues, the scanning strategies of the three scanning lidars are entirely user defined and could be optimized for turbulence measurements. Three scanning strategies were tested during LABLE II: a tri-Doppler technique, a six-beam technique (Sathe 2012), and a virtual tower technique (Calhoun et al. 2006).

In the first strategy, the tri-Doppler technique, the beams of the three scanning lidars were pointed to approximately the same point in space to avoid the use of a scanning circle. While the ARM Streamline DL operated in its standard vertical stare mode, the OU Streamline and Gabon DLs were steered toward a point 105 m above the ARM Streamline DL, which corresponds to the first useable range gate of the Streamline system. Since the radial wind speed is measured by three different lidars and there are three unknown wind components (v, v, and w), a set of three equations can be used to solve for the wind components. Although the effects of averaging within the probe volume cannot be mitigated in this way, the tri-Doppler technique allows for the measurement of turbulence within a small area of space rather than a large scanning circle and does not require the assumption of horizontal homogeneity within a scanning circle.

During LABLE II, the OU Streamline DL also evaluated a six-beam technique, which was developed by Sathe (2012) to minimize the variance contamination caused by the DBS technique. The final scanning strategy tested during LABLE II involved the use of all three scanning lidars to build a "virtual tower" over the WINDCUBE v2 lidar. This strategy was identical to the tri-Doppler technique, except the beams were moved to different heights every 10 min, forming a virtual tower with measurements at several different heights. Results from the six-beam and virtual tower measurements will be presented in separate publications that are currently in preparation.

Since one primary focus of LABLE was the comparison of turbulence parameters from different instruments, lidar quality control techniques were designed to optimize the accuracy of turbulence estimates. Two different methods were used to process the DL data and calculate variance. In the first technique, a spike filter developed by Hojstrup (1993) and adapted by Vickers and Mahrt (1997) was used to remove random noise from the raw lidar velocity time series. A 10-min moving window was shifted through the raw lidar data, and any point within the window that was more than 3.5 standard deviations from the mean was flagged as a possible spike and removed from the dataset. This process was repeated until no more spikes were detected. For each iteration of the spike filter, the factor of 3.5 standard deviations was increased by 0.1 standard deviation. The variance of each velocity component was then computed by averaging the 10-min variances over a 30-min period.

The second approach used the Lenschow technique (Lenschow et al. 2000), which assumes that noise is completely random and uncorrelated. Thus, in an autocovariance plot, the noise signal should spike at lag 0, then decorrelate immediately while the true atmospheric signal shows correlation beyond lag 0 in association with coherent motions. To estimate the amount of variance that is associated with noise, the raw velocity data were first detrended to ensure that the mean was zero. Next, the autocovariance function was calculated for each velocity component. Starting from lag 1, the autocovariance function was extrapolated back to lag 0 using a slope that is derived from the inertial subrange model. The value of the extrapolated function at lag 0 was then assumed to be the true variance, while the difference between the extrapolated function and the calculated function was assumed to be the variance due to noise.

For methods other than the Lenschow technique, SNR was also used to eliminate noisy lidar data. By default, WINDCUBE v2 radial velocities that were associated with SNR < -23 dB were not recorded in the output data stream. Similarly, Streamline and Galion DL radial velocities that were associated with SNR < -21 dB were removed from the dataset. Lidars are adversely affected by the presence of precipitation particles, which can result in beam attenuation and increased vertical velocities (e.g., Huffaker and Hardesty 1996; Pearson et al. 2009). Thus, lidar data were not used when the rain gauge at the ARM site recorded precipitation.

RESULTS. In the following, some initial results from the LABLE campaign are highlighted and discussed. Since assessing the performance of the different LABLE instruments is key to the scientific objectives of the project, instrument comparisons are presented first. As expected from previous studies (Bonner 1968; Song et al. 2005), LLJs frequently developed at night during LABLE, and the discussion in the remainder of this section focuses on LLJs. After a summary of general LLJ characteristics observed during LABLE I, the dynamic, thermodynamic, and turbulence structures of the NBL during two interesting LLJ events are compared. Finally, we highlight how the finescale structure of the NBL can be resolved using different scanning strategies with multiple DLs.

Instrument comparisons. Given the multilayered structure of the NBL, it is very important to have high-resolution profiles of wind, temperature, and turbulence parameters in the layer of the atmosphere influenced by the diurnal cycle (i.e., the layer from the ground up to a height of 2-3 km). Near the surface, observations with sonic anemometers coupled with infrared gas analyzers were proven to provide reliable data of mean wind and turbulent fluxes (Foken 2008). At the ARM SGP site, the instrumented 60-m tower and the nearby ECOR system provide such measurements at 4,25, and 60 m. The lowest reliable retrieval heights for the Streamline DLs are approximately 100 m, resulting in a data gap between 60 and 100 m that can often be filled in with observations from the sodar or the WINDCUBE v2 DL.

Sodars have been used to study the lower boundary layer since the 1970s (Coulter and Kallistratova 2004). The backscattered signal detected by sodars results from gradients in the temperature field caused by turbulent mixing (Hall et al. 1975; Anderson 2003). These structures in the temperature field are advected with the wind, so Doppler shifts in the received signals can be used to estimate properties of the wind field aloft. Doppler lidars, on the other hand, measure the Doppler shift of the backscattered energy from aerosol particles, which are assumed to be small enough to be tracers of atmospheric motion. DLs have been used in a wide range of ABL research, including studies of the CBL (e.g., Lothon et al. 2006; Traumner et al. 2011), LLJs in the nocturnal boundary layer (e.g., Banta et al. 2006), urban flow and turbulence characteristics (Newsom et al. 2008), and wakes behind wind turbines (Iungo et al. 2013; Barthelmie et al. 2014).

Given the differences in the measurement principles and possible error sources of the instruments used to construct continuous vertical ABL profiles, it is necessary to verify that their observations are consistent with each other. Data from overlapping measurement heights were thus selected and compared to identify and quantify possible instrument errors. For these comparisons, data were used for each full day of LABLE I in which there was at least 50% data availability from the sonic anemometer at 60 m. This resulted in a dataset consisting of 24 days during the experiment. Wind speed and direction measured by the sonic anemometer are provided as 30-min averages. Data from the sodar were used if the SNR from the vertical beam was greater than 3 dB. To assure a statistically robust comparison, 10-min averages of the cluster-analyzed wind components u and u were taken from the sodar and averaged onto the same 30-min periods as for the tower data. Wind speed and direction were then derived from the averaged u and u values. It should be noted that the spatial average represented by the tower's sonic anemometer and the sodar are vastly different. The sonic anemometer provides a point measurement. In contrast, the sodar uses the DBS technique to derive the horizontal wind components and as such involves a spatial average across the area captured by the five beams, equating to an area of approximately 110 [m.sup.2] at 60-m height.

Figure 3a depicts a comparison of the sodar-retrieved wind speeds at 60 m to those measured with the tower-mounted sonic anemometer at 60 m. The data are separated into day and night groupings, defined as 1330-2400 and 0030-1200 UTC, respectively (local time is UTC minus 5 h). Given the spatial sampling discrepancies, the wind speeds from the two instruments agree reasonably well. Also, there are no significant differences in the comparison statistics during the day versus at night with the [R.sup.2] values, where R is the Pearson correlation coefficient, being 0.83 for both day and night. The comparison of the wind directions (Fig. 3b), presented as a box-and-whisker plot of the differences between the wind direction measured by the sodar and sonic anemometer, grouped by wind speed, illustrates that a larger scatter in wind direction is observed for lower wind speeds, but for wind speeds [V.sub.T] > 5 m [s.sup.-1] (measured with the tower-mounted sonic anemometer at 60 m) the inner quartile range of the wind-direction differences is less than plus or minus 25[degrees].

The same type of comparison was also conducted between the sodar and OU Streamline DL retrievals of the horizontal winds at 90 and 160 m (Figs. 3c,d and 3e,f, respectively). The winds from the OU Streamline DL were measured at an elevation angle of 70[degrees] above the horizon, and the winds from the sodar were measured at an elevation angle of 72.2[degrees]. The DL wind profiles represent a 3-min average taken at 30-min increments, while the sodar wind profiles used for this comparison represent 10-min averages taken at 30-min increments. Note that the OU Streamline DL data from a lower elevation angle (e.g., 40[degrees]) could have been compared against the sodar data, but we chose to compare data from similar elevation angles and thus similar spatial averaging volumes.

Fewer samples are available for the 160-m comparison because the maximum retrieval height of the sodar was sometimes below 160 m. Unlike the 60-m sodar-sonic anemometer comparison, the [R.sup.2] values for the lidar-sodar comparison are different at night and day, but the differences are quite small and the trends are not consistent for the two measurement heights. The scatter in the lidar-versus-sodar wind speed comparison for both wind speed and wind direction is higher than in the tower-versus-sodar comparison but a clear bias of one instrument versus the other could not be identified. The different averaging times for the two instruments will likely be one factor contributing to the higher scatter but it should also be noted that the 90-m measurement level is pushing the lower limit of reliable data for the OU Streamline DL, while 160 m is at the upper limit (or above depending on the conditions) of the sodar measurement range.

To evaluate the skill of the AERI observations in providing information about the temperature structure in the lowest 1 km of the ABL, the mean bias and root-mean-square error (RMSE) were computed by comparing temperature profiles from Atmospheric Emitted Radiance Interferometer optimal-estimation (AERIoe) retrievals (Turner and Lohnert 2014) with rawinsonde temperature profiles. The rawinsonde data were interpolated to the AERI grid heights; the current retrieval is configured to have 26 levels in the lowest 1000 m (the grid goes from 10-m resolution at the surface to 100-m resolution at 1 km). The analysis was separated into LABLEI and II, as different AERI systems were used for the two periods. In LABLE I, we applied the AERIoe retrieval to the operational AERI system, which is collecting spectral data at 30-s resolution. However, this instrument was not operating properly during LABLE II; thus, we applied the retrieval algorithm to the older AERI-01 instrument, which was running at 8-min resolution. All clearsky rawinsonde profiles from the four-times-daily releases during LABLE I and II were included in the analysis (120 profile comparisons during LABLE I and 106 during LABLE II). The bias is less than 0.4[degrees]C up to 300 m for both LABLE I and II, and the RMSE values are almost the same (Fig. 4a). Above 300 m, the bias changes slightly between the two periods, but in both experiments the absolute bias is less than 0.5[degrees]C for all heights below 1 km. Additionally, the temperature gradients between 10 and 100 m AGL, defined as dT/dz = ([T.sub.100] - [T.sub.10])/90 m, observed by the AERI and rawinsonde temperature profiles are also compared (Fig. 4b). The comparison illustrates that the AERI observations capture the near-surface temperature structure very well during both campaigns. A tendency for a low bias can be noted for LABLE I, particularly for strong stabilities at night. However, the overall good agreement between the AERI and rawinsonde observations shows that AERI observations can be used to monitor the near-surface temperature structure of the atmospheric boundary layer, which is very important for investigating the LLJ development in more detail (see also more details below). In the remainder of the paper, we use AERI along with DL observations to provide new insights into the interplay between the thermodynamic and turbulence structure in the NBL for selected cases.

Low-level-jet development The ARM SGP site is situated within a climatological maximum of LLJ occurrences (Bonner 1968; Song et al. 2005). During the LABLE I campaign period, LLJs with peak winds of at least 10 m [s.sup.-1] were observed on 20 nights. The LLJ typically developed shortly after sunset and dissipated in the early morning hours. However, the exact onset and dissipation times of the LLJ varied greatly on each individual night, often depending on synoptic conditions.

For a more detailed analysis of the LLJ evolution throughout the night, we determined the height of the LLJ nose [Z.sub.LLJ] and the wind speed [V.sub.LLJ] at the height of the jet nose for all nocturnal (0000-1200 UTC) wind profiles for which a wind speed maximum was detected within the height range of the OU Streamline DL during LABLE I (599 profiles in total). The determination of [Z.sub.LLJ] and [V.sub.LLJ] can be difficult when the nose of the LLJ (i.e., the LLJ wind speed maximum [V.sub.max]) is not well defined. An algorithm was developed that, for all profiles with strong shear above and below the LLJ nose, assigned [V.sub.LLJ] = [V.sub.max] and [Z.sub.LLJ] to the height [Z.sub.max], where [V.sub.max] was detected. If the shear is weak at [Z.sub.max], then [Z.sub.LLJ] is assigned to the lowest height beneath [V.sub.max] at which wind shear is less than 0.025 [s.sup.-1], and [V.sub.LLJ] is the wind speed at [Z.sub.LLJ].

As illustrated in Fig. 5, the strength of the LLJs varied between 2.5 and 40 m [s.sup.-1] with [V.sub.LLJ] [approximately equal to] 10 m [s.sup.-1] being most frequently observed (Fig. 5a). The distribution for [Z.sub.LLJ] shows two peaks: around 250 and 400-450 m (Fig. 5b). The heights and strengths of the LLJ appear to be correlated with stronger jets having a tendency to be deeper (Fig. 5d). However, there is significant scatter and we plan to investigate in more detail the factors that contribute to this scatter utilizing the information from the AERI temperature profiles. An important objective of LABLE was the investigation of the turbulence regimes associated with LLJs. The standard deviation of the vertical velocity [[sigma].sub.w] can be considered an important characteristic for the intensity of vertical mixing in the NBL. The normalized mean ratios [[sigma].sub.w]/[V.sub.LLJ] below the LLJ nose peaked at around 0.02 but the values ranged from 0 to 0.1 (Fig. 5c). This large range in the normalized standard deviations of vertical velocity indicates that the turbulence structure can be very different for LLJs of comparable strength.

To highlight which factors may contribute to the differences in the NBL structure during LLJ events, we selected two interesting events, which are compared in Figs. 6-8. The two LLJ cases discussed here occurred on the mornings of 9 and 24 October 2012. In each instance, the LLJ was associated with an 850-hPa low pressure area to the northwest of the ARM SGP site. Both jets were of similar magnitude, with peak nocturnal winds recorded by the OU Streamline DL of approximately 24 m [s.sup.-1] on 9 October and 27 m [s.sup.-1] on 24 October. Figure 6 shows temperature, wind, and vertical velocity variance profiles observed at around 1130 UTC when rawinsonde observations were made during both nights. The profile comparisons demonstrate that the DL and sodar observations agree well with the rawinsonde profiles and sonic anemometer observations. Close to the ground, the AERI observations also agree well with the rawinsonde profiles, but at the height of the LLJ nose differences on the order of 2[degrees]C can be noted, which could be significant for assessing the bulk stability of the layer below the LLJ nose (see next paragraph). On the other hand, the distinct differences in the thermodynamic boundary layer structure during both nights are well captured by the AERI. Figure 6 illustrates that while the LLJ kinematics are quite similar at this hour during both nights the thermodynamic and turbulence structures for the two LLJ events had distinct differences. On 24 October the LLJ is associated with strong vertical mixing (Fig. 6f) and a very weak inversion near the surface (Fig. 6d); on 9 October a strong surface-based inversion developed (Fig. 6a) and turbulent mixing below the nose of the LLJ is absent (Fig. 6c), but gravity waves with strong rising-sinking motion couplets intermittently contributed to high [[sigma].sup.2.sub.w] values above 400 m at around 0500-0700 UTC (Fig. 7e). During both nights, the DLs reported lower [[sigma].sup.2.sub.w] values than did the sonic anemometers (Figs. 6c,f), which may be due to the larger probe volume of the DLs, but the different height ranges of the DLs and sonic anemometers prevent a direct, more detailed comparison.

Differences can also be noted in the onset of the LLJ development; while the LLJ developed quickly and remained relatively constant in magnitude after sunset on 24 October as the 850-hPa trough remained nearly stationary, the LLJ on 9 October developed more slowly as the winds increased overnight with the approach of the 850-hPa trough (Figs. 7a,b). Winds generally veered with height in the LLJ on both cases, and the winds became more westerly over time (Figs. 7c,d). While both LLJ events were of similar magnitude at their peaks, the LLJ on 24 October produced much stronger turbulent vertical mixing below the jet nose than the 9 October LLJ (Figs. 7e,f). In fact, significant mixing was maintained and increased over the entire night of 24 October (Fig. 8). It appears that because of the early onset of the LLJ (before a strong nocturnal inversion formed) turbulent mixing prevailed even after sunset, which prevented a strong surface-based inversion to form. Using the bulk shear ([V.sub.LLJ]/[Z.sub.LLJ]) computed from the DL wind profiles and potential temperature gradient across the layer from the surface to the LLJ nose [([[theta].sub.LLJ] - [[theta].sub.sfc])/[Z.sub.LLJ]] determined from the AERI temperature profiles, a bulk Richardson number [Ri.sub.bulk] was computed according to

[Ri.sub.bulk] = g/[theta] ([[theta].sub.LLJ] - [[theta].sub.sfc])/[Z.sub.LLJ]/[([V.sub.LLJ]/[Z.sub.LLJ]).sup.2], (1)

where g is the gravitational acceleration and [theta] is the mean potential temperature in the layer from the surface to the height [Z.sub.LLJ]. On 24 October, [Ri.sub.bulk] remained below 0.1 almost throughout the entire night (Fig. 8b), further confirming that the layer below the LLJ nose was only weakly stable. In contrast, the LLJ developed much later on 9 October. Mechanical generation of turbulence below the LLJ nose was thus very weak or nearly absent at sunset and a strong surface-based inversion formed quickly after sunset, with [Ri.sub.bulk] reaching values as high as 0.25-0.3 (Figs. 7g,h and 8a), which corresponds to the [Ri.sub.bulk] threshold identified in previous studies for the transition to very stable boundary layers where turbulence becomes intermittent (Banta et al. 2003; Mahrt 1999). As mentioned above, uncertainties in the AERI temperature observation at [Z.sub.LLJ] affect the accuracy of the [Ri.sub.bulk] values, but [Ri.sub.bulk] values computed from AERI and rawinsonde profiles at 0600 and 1200 UTC correlated very well with aslope of 0.91 for the AERI relative to the rawinsonde [Ri.sub.bulk] values. Individual values such as the spike around 1100 UTC October 24 (Fig. 8b) might be questionable ([Ri.sub.bulk] computed using temperature data from the rawinsonde at 1200 UTC was 0.09), but the overall trends are well captured by the AERI data and it is clear that the atmospheric stability below the LLJ was very different during the two episodes. With the inversion in place by the time winds increased to greater than 20 m [s.sup.-1], the strong static stability suppressed any mechanical generation of turbulence by the LLJ. Consequently, with less mixing, it is plausible that the LLJ was narrower and shear below the LLJ nose was stronger in the 9 October case compared with the 24 October LLJ (Figs. 7 and 8). The water vapor mixing ratio (r) data from the Raman lidar observations (Figs. 7i,j) show that the LLJ on 24 October was associated with much higher atmospheric humidity throughout approximately the lowest 1 km than on 9 October.

High-resolution lidar observations. As discussed in the previous sections, horizontal wind speed can be accurately measured with DLs. However, the temporal resolution is reduced as a result of the time it takes to perform a PPI scan, and it is difficult to obtain accurate turbulence statistics from PPI scans. During LABLE II we used a tri-Doppler technique that provides all three velocity components at 1-s temporal resolution. We used these measurements to construct 30-s-averaged wind profiles, which were compared against traditional VAD analysis profiles that were collected every 30 min by the ARM Streamline DL (Figs. 9 and 10) for 13 June 2013 when a strong LLJ developed that was lifted by the passage of a frontal boundary. The general LLJ evolution and its interaction with the mesoscale frontal boundary are well captured by the single DL VAD measurements (Figs. 9b,d), but only the high-resolution observations with the two horizontally staring DLs (Figs. 9a,c) capture the high-frequency oscillations in the wind field that developed as the LLJ was lifted by the front.

The reconstructions of the wind profiles from the two horizontal lidar stares (dual-Doppler analysis) require that measurements from different range gates from the two DLs be combined (the lidar beams intersect perfectly only at z = 105 m AGL but will be focused at different x and y coordinates for the other heights), which could potentially lead to discrepancies in the wind profiles. As shown in Fig. 10, the dual-Doppler mean wind profiles compare very well with the VAD profile measurements from both the ARM Streamline DL and the Leosphere WINDCUBE v2.

The high-resolution measurements were then also used to evaluate the Leosphere WINDCUBE v2 measurements of turbulence statistics. Time series of 30-min-averaged velocity variances [[sigma].sup.2.sub.u], [[sigma].sup.2.sub.v], and [[sigma].sup.2.sub.w], and turbulence kinetic energy (TKE) from 13 June 2013 are shown in Fig. 11. While the TKE measurements from the Leosphere WINDCUBE v2 generally agree well with the tri-Doppler data, some differences can be noted in the individual velocity variances. The WINDCUBE values for [[sigma].sup.2.sub.v] are consistently higher than the tri-Doppler data, which indicates that variance contamination by cross components of the Reynolds stress tensor (Sathe and Mann 2012) affects the WINDCUBE v2 measurements. However, the results for [[sigma].sup.2.sub.u] and [[sigma].sup.2.sub.w] show less-clear trends and further investigations are necessary to determine what causes the both higher and lower values of the WINDCUBE v2 variances compared to the tri-Doppler results. The accuracy of velocity variance and TKE measurements with different DL scanning techniques is currently further evaluated using turbulence parameters computed from 60-Hz sonic time series collected during the Lower Atmospheric Thermodynamics and Turbulence Experiment (LATTE) at the Boulder Atmospheric Observatory in early 2014. During LATTE, sonic anemometers were deployed at six levels from 50 to 300 m AGL--an ideal range for the comparison with DL observations.

SUMMARY AND FUTURE WORK. Leveraging ongoing collaborations between researchers and instrumentation from various agencies, the OU BLISS group was able to deploy multiple DLs and a sodar during two campaigns at the ARM SGP site. Graduate students played a leading role in the design of the experiments, the deployment and operation of the instruments, and the scientific data analysis. The sodar and DL measurements were combined with measurements from existing instrumentation at the ARM site to create rich datasets, which capture the dynamic, thermodynamic, and turbulence structures of the ABL for a wide range of synoptic conditions.

Our results indicate generally good agreement between mean wind speeds and directions measured by the various instruments during the campaign, which allows us to aggregate data from different instruments into profiles that capture the dynamic ABL structure in the lowest 2-3 km at high resolution. Having wind, turbulence, and temperature (from the AERI) profiles at high temporal resolution is a unique aspect of the LABLE datasets and we are not aware of other studies that measured the dynamic, turbulence, and thermodynamic ABL structures below 1 km at similar resolution for extended time periods. We demonstrated that the AERI observations accurately capture the near-surface temperature gradients; that is, the thermodynamic structure of the surface layer can be studied at high temporal resolution. As shown in the analysis of several LLJ cases, such datasets can provide new insights into the interplay between the dynamic, thermodynamic, and turbulence structures in the NBL. The time of LLJ onset appears to play a critical role in the decay or persistence of turbulent mixing after sunset. We presented a summary of general LLJ characteristics and discussed interesting features of individual LLJ cases. A more in-depth analysis that focuses on correlations between LLJ and stability parameters was conducted by one of the graduate students as part of his Ph.D. research (Bonin 2015; Bonin et al. 2015). Also, the skill of DLs in measuring turbulence statistics using different scanning strategies was evaluated more systematically by another graduate student as part of her Ph.D. thesis (Newman 2015). The LABLE campaigns thus provided valuable datasets for multiple student projects, and we expect several additional journal articles to be published in the near future. Work is also under way to quantify the water vapor flux at the top of the CBL over a range of conditions, and the datasets are also used to study the spatial and temporal variability of turbulence and how this variability is linked to land use near the ARM site. Future work will also focus on additional case studies of cold fronts and gravity waves, incorporating data from ARM's K-, X-, and C-band radars, which provide valuable scans over the site to potentially complement observations made by the other instruments mentioned in this paper. The LABLE DL and sodar observations, as well as AERIoe retrievals, are available in the ARM archive.

ACKNOWLEDGMENTS. This research was supported by NOAA's National Severe Storms Laboratory and the Department of Energy's (DOE) Atmospheric System Research (ASR, Grant DE-SC0006898) program. The OU lidar was purchased using funds from the NSF Career Award ILREUM (NSF ATM 0547882) and the Office of the Vice President for Research at the University of Oklahoma. The OU sodar was purchased using funds from the NSF (NSF AGS 1229181). The rental of the Galion DL and the loan of the WINDCUBE v2 were provided by a grant with Lawrence Livermore National Laboratory (Project 130180). These grants also provided funding for the majority of the authors. In addition, SW was funded by an LLNL Laboratory Directed Research and Development (LDRD) grant (12-ERD-069). We thank Matthieu Boquet, Mehdi Machta, and the rest of the Leosphere team for generously loaning their lidar to us for this project and for their support during and after the experiment. We are also grateful for the support of the SGURR Energy team around Gareth Brown and Nick Capaldo in the setup of the Galion DL and data processing. The ARM data used in this paper were collected by the DOE Atmospheric Radiation Measurement (ARM) program and are available via its data archive ( We would also like to thank the ARM SGP staff for their support during the campaign.

AFFILIATIONS: Klein, Bonin, Newman, Wainwright, Carney, and Jacobsen-School of Meteorology, University of Oklahoma, Norman, Oklahoma; Turner-NOAA/National Severe Storms Laboratory, Norman, Oklahoma; Chilson-School of Meteorology, and Advanced Radar Research Center, University of Oklahoma, Norman, Oklahoma; Blumberg-School of Meteorology, and Cooperative Institute for Mesoscale Meteorological Studies, University of Oklahoma, Norman, Oklahoma; Mishra-Cooperative Institute for Mesoscale Meteorological Studies, University of Oklahoma, Norman, Oklahoma; Wharton-Lawrence Livermore National Laboratory, Livermore, California; Newsom-Pacific Northwest National Laboratory, Richland, Washington

CORRESPONDING AUTHOR: Dr. Petra Klein, School of Meteorology, University of Oklahoma, 120 David L. Boren Blvd., Norman, OK 73072


The abstract for this article can be found in this issue, following the table of contents.

DOI: 10.1175/BAMS-D-13-00267.1


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The Atmospheric Emitted Radiance Interferometer (AERI) is an operational ground-based spectrometer that measures the downwelling infrared (3-19 [micro]m) radiance emitted by the atmosphere at a high temporal and spectral resolution (Knuteson et al. 2004a).These spectra, examples of which are shown in Fig. SB 1, provide a wealth of information on the state of the atmosphere above the instrument. Data from the AERI have been used in a wide range of analyses, including for characterizing the evolution of the thermodynamic structure of the lower troposphere (e.g., Feltz et al. 1998; Feltz et al. 2003), quantifying the microphysical properties of clouds (e.g., Mace et al. 1998; Comstock et al. 2007; Turner 2007) and aerosols (e.g., Turner 2008), providing estimates of trace gas concentrations in the column (e.g., Yurganov et al. 2010), and improving the accuracy of spectroscopic radiative transfer models (e.g., Tobin et al. 1999; Turner et al. 2004; Mlawer et al. 2012).

The spectral signature of the down-welling radiance contains information on the vertical profile of temperature and water vapor, as illustrated by the differences among the temperature and water vapor (Fig. SB 1c) profiles associated with the three observed spectra (Fig. SB 1a).Trace gases such as carbon dioxide, ozone, methane, and, of course, water vapor have many absorption lines in the portion of the infrared spectrum observed by the AERI (Fig. SB 1b), and clouds and aerosols are easily observed in the 8-12-[micro]m atmospheric window. Retrieval algorithms, such as the one by Turner and Lohnert (2014), use portions of the observed spectrum to derive information on the atmospheric profiles. The strong carbon dioxide absorption band centered at 15 [micro]m, which is composed of hundreds of absorption lines of various strengths and thus optical depths, provides information on the temperature profile, with AERI channels associated with more opaque absorption features providing information closer to the instrument (i.e., near the surface) and more transparent channels providing information aloft. Similarly, a large number of AERI channels where water vapor is the primary absorbing gas (note that there are many spectral regions where multiple gases absorb radiation simultaneously and these regions are typically not used in retrieval algorithms) are used to provide the profile of water vapor. Clouds are a strong emitter of infrared radiation, and thus retrieval algorithms are built to simultaneously retrieve thermodynamic profiles and cloud properties (e.g., Turner and Lohnert 2014).

As with any ground- or space-based passive remote sensor, accurate calibration is critical, as any bias in the observed radiance results in significant errors in the retrieved atmospheric properties. The AERI regularly views two blackbodies that have well-characterized emissivity characteristics and accurate thermistors embedded to provide a radiometric calibration that is better than 1% of the ambient radiance (Knuteson et al. 2004b).The calibration stability of this instrument not only enables accurate thermodynamic profiling, but also long-term trend analysis of downwelling radiance (Gero and Turner 2011).

Table 1. Overview of the instrumentation deployed during the LABLE
field campaigns (names of graduate students serving as co-primary
investigators (Pis) are italicized in the second column).

Instruments/platform                    Owner/operator/deployment

Gill Solent Windmaster Pro 3D       ARM/Lawrence Berkeley National
sonic anemometer and Licor          Laboratory/continuous
Infrared Gas Analyzer/60-m tower
and ECOR system *

Vaisala HMP45D/60-m tower           ARM/Argonne National Laboratory/

Vaisala 50Y Humitter/ECOR system    ARM/Lawrence Berkeley National

AERI                                ARM/ARM/continuous

Raman lidar                         ARM/ARM/continuous

Vaisala RS92 rawinsondes            ARM/ARM/regularly every 6 h
                                    (0000, 0600, 1200, and 1800 UTC)

OU Metek sodar                      OU/P. Chilson and C.
                                    Wainwright/LABLE 1

ARM Streamline DL                   ARM/Pacific Northwest National

OU Streamline DL                    OU/P. Klein and T. Bonin/LABLE 1
                                    and II

Galion DL                           SGURR Energy/P. Klein, T. Bonin,
                                    and J. Newmon/LABLE II

LeosphereWINDCUBE 200               Leosphere/D.Turner/LABLE 1

LLNL Leosphere WINDCUBE v2          LLNL/S. Wharton and J.
                                    Newmon/LABLE II

Instruments/platform                      Available data output

Gill Solent Windmaster Pro 3D       30-min averages of V, (WD),
sonic anemometer and Licor          [T.sub.s], and vertical fluxes of
Infrared Gas Analyzer/60-m tower    momentum, C[O.sub.2], sensible
and ECOR system *                   heat, and latent heat **

Vaisala HMP45D/60-m tower           1-min time series of T and RH

Vaisala 50Y Humitter/ECOR system    30-min time series of T and RH

AERI                                Downwelling IR radiance spectra
                                    every 20 s; Retrieved temperature
                                    and humidity profiles every 5 min

Raman lidar                         Backscatter data in multiple
                                    channels at 7.5-m, 10-s
                                    resolution; water vapor profiles
                                    at 75-m, 10-s resolution

Vaisala RS92 rawinsondes            Vertical profiles of atmospheric
                                    pressure p, RH, and T

                                    Wind speed and direction
                                    determined using GPS

OU Metek sodar                      10-min averages of power, SNR,
                                    and radial velocities, which are
                                    used to calculate 3D wind

ARM Streamline DL                   ~1 -Hz radial velocities,
                                    VAD-derived horizontal wind every
                                    15 min, [[sigma].sub.w'] usually
                                    averaged over 30 min

OU Streamline DL                    ~1 -Hz radial velocities,
                                    VAD-derived horizontal wind
                                    (frequency varied),
                                    [[sigma].sub.w] usually averaged
                                    over 30 min

Galion DL                           ~1 -Hz radial velocities, outputs
                                    varied based on different scan
                                    strategies during LABLE II

LeosphereWINDCUBE 200               Carrier noise ratio (dB),
                                    vertical velocity (m [s.sup.-1]),
                                    and vertical dispersion
                                    (m [s.sup.-1]) profiles (this
                                    system only stared vertically)

LLNL Leosphere WINDCUBE v2          u, [upsilon], and w at 1 Hz

Instruments/platform                          Specifications

Gill Solent Windmaster Pro 3D       H = 4, 25,60 m
sonic anemometer and Licor
Infrared Gas Analyzer/60-m tower    Range: 0 to 65 m [s.sup.-1] (V),
and ECOR system *                   -40[degrees] to +60[degrees]C

                                    Accuracy: 1.5% RMSE for u and v,
                                    3% RMSE for w, 3% error in speed
                                    of sound for Ts

                                    Resolution: 0.01 m [s.sup.-1]
                                    (V), 0.02[degrees]C ([T.sub.s])

                                    Flux detection limits: C[O.sub.2],
                                    ~0.1 [micro]mol [m.sup.-2]
                                    [s.sup.-1]; gain uncertainty, l%
                                    to 3%; [H.sub.2]O, ~10 W
                                    [m.sup.2]; gain uncertainty, 1%
                                    to 3%; sensible heat, ~10 W
                                    [m.sup.-2]; gain uncertainty, 1%
                                    to 3%

Vaisala HMP45D/60-m tower           H = 25,60 m

                                    Range: -30[degrees] to
                                    40[degrees]C (T), 0% to 100% (RH)

                                    Accuracy: [+ or -] 0.2[degrees]C
                                    (T), [+ or -] 2% up to 90% (RH),
                                    [+ or -] 3% above 90% RH

Vaisala 50Y Humitter/ECOR system    H = 2, 3 m

                                    Range: -10[degrees] to
                                    60[degrees]C (T), 0% to 100% (RH)

                                    Accuracy: [+ or -] 0.6[degrees]C
                                    (T),from +2% to [+ or -] 3% (RH)

AERI                                Spectral range: 520-3000
                                    [cm.sup.-1] at 1.0-[cm.sup.-1]

                                    Accuracy: better than 1 % of the
                                    ambient radiance

                                    Thermodynamic profiling range:
                                    surface to ~3 km

                                    Accuracy of temperature profile:
                                    better than 0.5 K

Raman lidar                         Laser wavelength: 0.355 [micro]m

                                    Pulse repetition rate: 30 Hz

                                    Accuracy of the water vapor
                                    profiles in lowest 4 km: 5% or
                                    0.5 g [kg.sup.-1], whichever is

Vaisala RS92 rawinsondes            Range: 0% to 100% (RH),
                                    -90[degrees] to +60[degrees]C
                                    (T), 1080 to 3 hPa (p)

                                    Uncertainty: 5% (RH),
                                    0.5[degrees]C (T)

                                    Resolution: 1 % (RH),
                                    0.1[degrees]C (7), 0.1 hPa (p)

OU Metek sodar                      H = 30 to 500 m

                                    Range resolution: 10 m

                                    Accuracy--wind direction:
                                    [+ or -] 5[degrees]

                                    Wind speed: [+ or -] 0.5 m
                                    [s.sup.-1] (below 5 m [s.sup.-1])
                                    and [+ or -] 10% above 5 m

ARM Streamline DL                   H = 100 to 3000 m

                                    Range resolution: 30 m

                                    Range: [+ or -] 19.4 m [s.sup.-1]
                                    (Nyquist velocity)

                                    Resolution: <20 cm [s.sup.-1] for
                                    SNR > -17 dB

                                    Wavelength: 1.5 [micro]m

                                    Pulse repetition rate: 15 kHz

OU Streamline DL                    H = 100 to 3000 m (technically
                                    can collect data out to 9.6 km)

                                    Range resolution: 18 m

                                    Range: [+ or -]  19.4 m
                                    [s.sup.-1] (Nyquist velocity)

                                    Resolution: <20 cm [s.sup.-1] for
                                    SNR > -17 dB

                                    Wavelength: 1.5 [micro]m

                                    Pulse repetition rate: 15 kHz

Galion DL                           H = 80 to 4000 m

                                    Range resolution: 30 m

                                    Range: [+ or -] 38.8 m [s.sup.-1]
                                    (Nyquist velocity)

                                    Resolution: <20 cm [s.sup.-1] for
                                    SNR > -17 dB

                                    Wavelength: 1.5 [micro]m

                                    Pulse repetition rate: 15 kHz

LeosphereWINDCUBE 200               Temporal resolution: 4 s

                                    Vertical resolution: 50 m

                                    Resolution: <20 cm [s.sup.-1]

                                    Wavelength: 1.5 [micro]m

                                    Pulse repetition rate: 20 kHz

LLNL Leosphere WINDCUBE v2          H = 40 to 200 m

                                    Range resolution: 20 m

                                    Range: [+ or -] 60 m [s.sup.-1]

                                    Accuracy: 0.1 m [s.sup.-1]

                                    Wavelength: 1.5 [micro]m

                                    Pulse repetition rate: 20 kHz

* The measurements at 4 m AGL are taken at the ECOR system site (E);
the 25- and 60-m data are collected at the 60-m tower (T).

** For our analysis, we used a data stream with 30-min-averaged
fluxes, which are computed using 10-Hz time series of the wind
velocity components u, v, and vv; sonic temperature [T.sub.s]
measured by the sonic anemometer; and C[O.sub.2] and [H.sub.2]O
densities measured by the infrared gas analyzer.The data stream also
includes additional variables such as Obukhov length L and friction
velocity [u.sub.*].
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Author:Klein, P.; Bonin, T.A.; Newman, J.F.; Turner, D.D.; Chilson, P.B.; Wainwright, C.E.; Blumberg, W.G.;
Publication:Bulletin of the American Meteorological Society
Article Type:Report
Geographic Code:1U7OK
Date:Oct 1, 2015
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