Journal cover Journal topic
Wind Energy Science The interactive open-access journal of the European Academy of Wind Energy
Journal topic
Wind Energ. Sci., 3, 203-219, 2018
https://doi.org/10.5194/wes-3-203-2018
Wind Energ. Sci., 3, 203-219, 2018
https://doi.org/10.5194/wes-3-203-2018

Research articles 25 Apr 2018

Research articles | 25 Apr 2018

# Investigating the impact of atmospheric stability on thunderstorm outflow winds and turbulence

Downburst winds during the evening transition
Patrick Hawbecker1, Sukanta Basu2, and Lance Manuel3 Patrick Hawbecker et al.
• 1Department of Marine, Earth, and Atmospheric Sciences, North Carolina State University, Raleigh, NC 27695, USA
• 2Faculty of Civil Engineering and Geosciences, Delft University of Technology, Delft, the Netherlands
• 3Department of Civil, Architectural, and Environmental Engineering, University of Texas at Austin, Austin, Texas 78712, USA
Abstract

Downburst events initialized at various hours during the evening transition (ET) period are simulated to determine the effects of ambient stability on the outflow of downburst winds. The simulations are performed using a pseudo-spectral large eddy simulation model at high resolution to capture both the large-scale flow and turbulence characteristics of downburst winds. First, a simulation of the ET is performed to generate realistic initial and boundary conditions for the subsequent downburst simulations. At each hour in the ET, an ensemble of downburst simulations is initialized separately from the ET simulation in which an elevated cooling source within the model domain generates negatively buoyant air to mimic downburst formation.

The simulations show that while the stability regime changes, the ensemble mean of the peak wind speed remains fairly constant (between 35 and 38 m s−1) and occurs at the lowest model level for each simulation. However, there is a slight increase in intensity and decrease in the spread of the maximum outflow winds as stability increases as well as an increase in the duration over which these strongest winds persist. This appears to be due to the enhanced maintenance of the ring vortex that results from the low-level temperature inversion, increased ambient shear, and a lack of turbulence within the stable cases. Coherent turbulent kinetic energy and wavelet spectral analysis generally show increased energy in the convective cases and that energy increases across all scales as the downburst passes.

1 Introduction

Severe thunderstorms producing tornadoes and extreme winds have garnered a lot of attention in the wind engineering and wind energy communities due to the high risk of structural damage to buildings and wind turbines caused by these events. In 2016 alone, severe thunderstorms caused an estimated USD 14 billion in insured losses within the United States, roughly 60 % of the total estimated insured losses from natural catastrophes for the year (source: 2017 Munich Re as of February 2017). Historically, there have been several instances of structures directly impacted by these events, resulting in studies focused on estimating the loads generated by these winds on structures such as buildings  and electricity transmission towers . With the recent growth of the wind energy industry, the occurrence of severe winds impacting wind turbines has become more common. For example, footage of a tornado moving through a wind farm in Harper County, Kansas, which occurred in 2012 shows the blades of a wind turbine being stripped away and projected (source: https://www.youtube.com/watch?v=Egdtlnv6Gio, last access: 19 April 2018), while a severe thunderstorm event that struck the Buffalo Ridge Wind Farm in 2011 ended up causing several wind turbines to lose their blades and the buckling of a tower . Traditionally, surveys of damage done to features such as buildings, crops, and trees are conducted after an event and, based on the severity of the damage, a rating of 1–5 is assigned based on the Enhanced Fujita (EF) scale , formerly known as the Fujita scale (Fujita1971, 1981). The EF scale uses damage–wind relationships and bases the ratings on observed damage and design codes. However, indirect estimation of extreme winds based on damage surveys and damage–wind relationships is known to be imprecise and uncertain at times ; still, due to the dearth of high-density wind measurement networks, the wind engineering community is compelled to use these estimations. In recent years, high-resolution numerical modeling is gaining momentum as a viable alternative that can serve as a surrogate to in situ data .

While high-resolution observations of near-surface winds for severe wind events are rare, climatologies of severe wind events have been developed via several intensive field campaigns and by utilizing storm reports from the National Weather Service (NWS). One such climatology of thunderstorms producing severe winds over the contiguous United States was developed about three decades ago by . This climatology is generated based on NWS storm reports of thunderstorm-related wind damage over a 29-year period from 1955 through 1983 but it is impossible to distinguish the storm type (i.e., downburst, derecho, rear flank downdraft) from these reports. Around the same time, generated another storm climatology based solely on observed downbursts from the Joint Airport Weather Studies (JAWS) project . Even though the size of the analyzed dataset was much smaller than that of , was able to document the circadian traits of downbursts. Figure 1a shows a regenerated version of the data from Fig. 6 in while Fig. 1b shows the regenerated data from Fig. 4 in . Here, it can be seen that severe wind events occur most often during the late afternoon. As the sun begins to set, the number of severe wind events begins to sharply decrease. However, late evening and even nocturnal events, while less common, do occur for all wind events (Fig. 1a) and downbursts (Fig. 1b).

The period of the day roughly 2 h before sunset to 2 h after sunset is known as the evening transition (ET), when, in a matter of hours, the atmospheric boundary layer (ABL) transitions from the daytime convective boundary layer (CBL) to the nighttime stable boundary layer (SBL). The CBL is characterized by large turbulent eddies spanning the depth of the boundary layer generated from the heating of the surface. As the sun sets and the surface begins to cool, the SBL develops where a surface-based layer of stably stratified air forms along with an increase in low-level vertical wind shear. Further, due to the lack of surface heating, the turbulence from large convective eddies is greatly reduced (Stull1988). The neutral boundary layer (NBL) exists only very briefly between the convective and stable regimes  where vertical sensible heat flux near the surface is zero and there is an adiabatic lapse rate throughout the boundary layer (Stull1988). At the beginning of the ET, when the boundary layer is still in a convective state, solar heating is able to generate convective instabilities in the boundary layer that can initiate thunderstorms (Wakimoto2001). However, as the sun sets, this convective instability source is lost, thus decreasing the number of such severe events.

Another interesting observation can be made from Fig. 1a: as the atmospheric stability increases during the ET, the percentage of events considered strong or violent remains relatively constant. In other words, atmospheric stability does not seem to play a role in modulating the ratio of severe to non-severe wind events. This counterintuitive result should be studied in detail. In fact, the impact of increased stability on tornadogenesis has been investigated recently; the climatologies of tornadic events have suggested a peak in the occurrence frequency of tornadoes in the early evening . In the present study, we will probe further into how stability impacts downburst winds and into such implications on the wind energy and wind engineering communities. Other extreme wind events (derechos, rear flank downdrafts, etc.) are out of scope of the present study.

Downbursts, defined as such by , produce low-level diverging outflow capable of generating severe winds. Such outflow is dominated primarily by the horizontal components of the wind field; however, they are enhanced by strong vertical motions at low levels as well. Downbursts are typically associated with thunderstorm activity and are commonly separated into two categories: dry and wet (Wakimoto1985). Dry downbursts are associated with little or no rain at the surface during the outflow winds. In contrast, wet downbursts are associated with rainfall at the surface during the time of the outflow winds. In order to understand distinctions between a downburst classified as dry or wet and the potential impact of atmospheric stability on downburst winds, basic concepts of downburst formation are explained here. The two main drivers to generate a downburst are hydrometeor loading (i.e., drag from falling hydrometeors) to initiate the sinking motion and latent cooling from melting, evaporation, and sublimation of the hydrometeors (Wakimoto2001). These produce a pocket of cold (relative to the environment), negatively buoyant air that descends towards the surface and spreads out laterally as it reaches the ground. With that basic picture in mind, several factors (e.g., the ambient turbulent motions of the CBL or the surface inversion with increased low-level wind shear in the SBL) play a role in modifying the downburst winds. For example, in a typical CBL or NBL regime, the pocket of air would remain negatively buoyant throughout its descent to the surface. However, in the SBL, where a low-level inversion is present, the downburst air could become less negatively buoyant (or even positively buoyant) as it descends through the low-level stable layer (Proctor1989). Since the resulting horizontal wind speeds are a function of the maximum downdraft velocity, wmin, if wmin is smaller (larger) then the outflow wind speeds will in turn be smaller (larger) . Thus, if the downdraft encounters a highly turbulent environment, the mixing and entrainment of ambient environmental air can weaken the negative buoyancy of the parcel and, in turn, decrease the outflow wind speeds.

Figure 1(a) The frequency of wind gusts of varying severity throughout the day (solid lines) overlaying the percentage of each wind gust severity category. Red, yellow, and green coloring correspond to violent gusts (greater than 33.5 m s−1), strong gusts (between 25.8 and 33.5 m s−1), and events with reported damage but no estimated wind speeds, respectively. Data have been adapted from , where the times have been converted to normalized solar time (NST). (b) Time of occurrence of the downbursts observed in the JAWS campaign; regenerated data from Fig. 4 in .

For several decades, the wind engineering and the atmospheric science communities have studied downburst winds. Due to a lack of high-resolution low-level observations during these events, as previously mentioned, numerical models as well as laboratory experiments (Jesson et al.2015; Lundgren et al.1992; Sengupta and Sarkar2008; Yao and Lundgren1996; Zhang et al.2013) have been utilized to study downburst dynamics and wind fields. Numerical models employed include analytical models, Reynolds-averaged Navier–Stokes (RANS) models, large eddy simulation (LES) models, and mesoscale meteorological models.

Initially, based on observations, analytical models were developed in order to assess the danger of downbursts to aircrafts . Such studies were, in a large part, motivated by several commercial airline accidents (e.g., the Delta Airlines Flight 191 crash at Dallas–Fort Worth in 1985 with 137 fatalities; ) and an earlier high-profile near miss at Andrews Air Force Base in 1983 in which Air Force One carrying then President Reagan landed just 6 min before wind speeds had reached 67 m s−1 at 5 m above the surface (Fujita1985). Developments stemming from these early analytical models proved to be useful in wind engineering studies  and to wind energy research . These relatively simple models are very efficient and inexpensive to run at high resolution, making them the state of practice in the wind engineering community. However, these models fall short of representing the underlying physics accurately and, especially with regard to turbulence, they rely on synthetically generated stochastic fields associated with target power spectral density functions, which are not specifically associated with downbursts.

RANS simulations of downburst winds  and LES studies  both solve the Navier–Stokes equations and have been used to study the dynamics of downburst winds. What separates the two methods is that RANS models estimate the entire turbulent contributions of the flow field, while LES resolves the largest turbulent eddies and parameterizes only the smaller turbulent eddies. An advantage of both approaches is that several fundamental physical features of downburst flows can be simulated. For example, RANS studies performed by produced, to the best of our knowledge, the first simulation of what is known as the “ring vortex” – a distinctive feature commonly observed in downbursts . This feature is characterized by the rotation (roll-up) around a horizontal axis located towards the edge of the outflow and commonly associated with the strongest outflow winds. Further, the influence of various other factors such as terrain , the interactions of colliding downburst outflows , and the microphysics and ambient humidity  have all been explored. Full-storm simulations utilizing advanced parameterizations  are now able to help us advance our knowledge of downburst dynamics and study these various influences. A major drawback of RANS, LES, and full-storm simulations is the computational expense involved in obtaining high-resolution spatiotemporal representations of downbursts. As a result, these models are rarely run at resolutions suitable for use as inflow in engineering models.

To the best of our knowledge, all previously published numerical studies of downburst winds have only considered downbursts in the NBL with one exception – a sensitivity study by that used a RANS model. In that study, surface-based deep inversion layers of 500 and 1000 m were used to mimic nocturnal stability or the outflow of another storm. It was shown that the stable layer at the surface reduced the magnitude of the outflow wind speed and the maximum downdraft; it also prevented one downburst event from even reaching the surface entirely. The height of the ring vortex that formed was also shown to be sensitive to the surface-based inversion in that this height was equivalent to (or the same as) that of the stable layer. This single study only describes part of the influence of the SBL; the expected characteristic increase in low-level wind shear, a fundamental feature of the SBL, was ignored.

When considering the three planetary boundary layer (PBL) regimes, it is to be expected that initial studies would only consider neutral conditions. The NBL provides the most simplistic ambient environment in that it lacks several complex processes inherent to the CBL and SBL. However, since thunderstorms and downbursts occur throughout the night and day, it is necessary to assess what effect stability might have on downburst outflows. In the present study, a pseudo-spectral LES model with a dynamic sub-grid-scale (SGS) scheme is utilized to simulate downbursts in various stability regimes. The goal of this study is to analyze outflow wind fields to learn how downburst intensity and flow characteristics change with increased low-level stability. Section 2 introduces the methodology employed in this study. Results for the ET and the downburst simulations are presented in Sect. 3.1 and 3.2, respectively. Finally, a summary and conclusions are provided in Sect. 4.

2 Methods

Simulating the diurnal cycle has been a challenging topic in boundary layer meteorology for some time. In convective simulations, the model domain size must be large enough in both the horizontal and vertical extent to capture the convective processes. Due to these large domains, modelers are typically constrained to using relatively coarse grid sizes to decrease the computational burden of each simulation. However, when simulating the SBL, the model grid spacing and time step must be small enough to capture developing nighttime eddies that are on the order of meters. In order to satisfactorily simulate both regimes, a large model domain with small grid spacing is necessary; this results in the need for a large amount of computational grids. With advances in computational power, we have began to be able to run these types of simulations with relative ease.

used a dynamic SGS scheme, called the locally averaged scale-dependent dynamic (LASDD) model , to simulate a full diurnal cycle. The results showed good agreement with observations and, additionally, little dependence on model grid spacing. In the LASDD SGS model, the SGS coefficients are computed dynamically based on the local dynamics of the flow, whereas in typical SGS schemes the SGS coefficients are specified in an ad hoc manner.

The LES model used in  is utilized here to simulate the idealized downbursts. The model forcing is imposed by specifying the geostrophic wind and the surface temperature. The model domain spans 10 km in both lateral directions and 3 km in the vertical. The grid spacing is approximately 28 m in both the horizontal and vertical directions. The model's lateral boundaries are periodic in both the x and y direction, and a damping layer is employed on the top 1 km of the domain in order to eliminate reflections off of the model top. A roughness length of 0.1 m is utilized corresponding closely to the average roughness length over North America (Stull1988). The simulations of downbursts during the evening transition is conducted in three phases (Fig. 2).

Figure 2A schematic diagram depicting the process for simulating downbursts throughout the evening transition period. The first phase consists of model spin-up to generate the CBL. The second phase simulates the ET while outputting a snapshot every hour to be used as the initial and boundary conditions in the downburst simulations performed in Phase III. These snapshots are denoted as C1 for the moderately convective case, C2 for the weakly convective case, N for the neutral case, S1 for the weakly stable case, and S2 for the moderately stable case.

## 2.1 Phase I: spin-up simulation

The model is initialized with a neutral potential temperature profile up to the initial boundary layer height of 1.5 km and a constant geostrophic wind of 8 m s−1 in the positive-x direction (i.e., Ug=8.0 m s−1; Vg=0.0 m s−1). A prescribed surface temperature is used as the lower boundary condition to drive the flow. In this case, the initial temperature in the NBL is 300 K and the surface temperature is prescribed to be 303 K. For the first 2 h of the simulation, the constant surface temperature is used to develop the convective boundary layer. The model time step, Δt, is set to 0.5 s. These 2 h are regarded as the period of model spin-up and data from this phase are not used in subsequent analysis.

## 2.2 Phase II: ET simulation

In the second phase, the ET is simulated for 4 h, during which the surface temperature is decreased by 1.135 K h−1 such that after 2 h the boundary layer will reach a neutral state and the SBL will be developed in the subsequent 2 h. The selected surface temperature cooling rate was found by trial and error in order to produce a neutral state after 2 h of cooling. In this phase, the same Δt of 0.5 s is used as in Phase I and, after every hour of simulation, the full three-dimensional velocity and temperature fields are output to be used as initial and boundary conditions for Phase III simulations. These snapshots are denoted as C1 for the moderately convective case, C2 for the weakly convective case, N for the neutral case, S1 for the weakly stable case, and S2 for the moderately stable case; they are output at hours 0, 1, 2, 3, and 4, respectively.

Figure 3Vertical profiles of average wind speed (a), temperature (b), and normalized vertical sensible heat flux (c) are shown for the C1, C2, N, S1, and S2 cases colored red, yellow, gray, green, and blue, respectively. The normalized vertical sensible heat flux profiles are normalized with respect to the average surface sensible heat flux of the C1 simulation.

## 2.3 Phase III: downburst simulations

The downburst simulations are initialized from the C1, C2, N, S1, and S2 snapshots of the ET simulation. In these simulations, Δt is reduced to 0.1 s and each simulation is run for 15 min. This decrease in time step is made to ensure stability and for the collection of high-temporal-resolution data to be used in a follow-up study utilizing the Fatigue, Aerodynamics, Structures, and Turbulence (FAST) model. Due to the sensitivity of LES runs to initial conditions, an ensemble of simulations is generated for each stability case (C1, C2, N, S1, and S2). Each case is run four times; taking advantage of the periodic boundaries in the x- and y directions, the initial conditions generated from the ET simulation are shifted as follows: (1) in the x direction by +5 km (denoted by 5x_0y), (2) in the y direction by +5 km (denoted by 0x_5y), and (3) in both the x and y directions by +5 km (denoted by 5x_5y). Including the original initial conditions, this strategy results in four sets of initial conditions for each case. Shifting the initial conditions in this manner effectively initializes the downburst at different locations within the same ABL regime.

## 2.4 Downburst forcing

A cooling source near the top of the model originally proposed by  is used to produce negatively buoyant air to simulate the effects of latent cooling due to the melting, evaporation, and sublimation of hydrometeors as they descend towards the surface. These processes are largely responsible for generating the negative buoyancy that drives the downburst (Wakimoto2001) and this approach has become the state of the practice in LES simulations of downburst winds (see, for example, , or ). The source (Q) equations are as follows:

$\begin{array}{}\text{(1)}& Q\left(x,y,z;t\right)=\left\{\begin{array}{ll}{C}_{\mathrm{max}}×g\left(t\right){\mathrm{cos}}^{\mathrm{2}}\left(\mathit{\pi }R\right),& R\le \frac{\mathrm{1}}{\mathrm{2}}\\ \mathrm{0},& R>\frac{\mathrm{1}}{\mathrm{2}}\end{array}\right\,\end{array}$

where Cmax is the peak intensity of the cooling function and is set to 0.08 K s−1 as was done in and   to produce an intense downburst. The function, g(t), defines the variation of downburst intensity with time as follows:

$\begin{array}{}\text{(2)}& g\left(t\right)=\left\{\begin{array}{ll}{\mathrm{cos}}^{\mathrm{2}}\left[\mathit{\pi }\left(\frac{t-\mathrm{120}}{\mathrm{2}\mathit{\tau }}\right)\right],& \mathrm{0}

where τ is set to 120 s. Equation (2) differs from previous studies in that the cooling source is held constant for 2 min, as opposed to 10 min. This is done in order to analyze the decay of the downburst events before they reach the simulation boundary as well as to limit the source from generating multiple strong downburst events. Finally, R represents the normalized distance from the center of the cooling function :

$\begin{array}{}\text{(3)}& R=\sqrt{\left(\frac{x-{x}_{f}}{{M}_{x}}{\right)}^{\mathrm{2}}+\left(\frac{y-{y}_{f}}{{M}_{y}}{\right)}^{\mathrm{2}}+\left(\frac{z-{z}_{f}}{{M}_{z}}{\right)}^{\mathrm{2}}}.\end{array}$

Here, the coordinates of the center of the downburst, $\left({x}_{f},{y}_{f},{z}_{f}\right)$, are set to (2.5, 5.0, 1.9 km). The x position is chosen so as to allow the downburst to reach the surface near the center of the domain and extend the amount of time before the downburst reaches the model boundary. The vertical location of the cooling center is chosen such that it is concentrated just inside the entrainment zone overlying the mixed layer. The horizontal and vertical extent of the cooling source, defined by Mx, My, and Mz, are set to 2.0, 2.0, and 1.5 km, respectively, such that the vertical extent of the cooling source does not reach the surface. This type of cooling source essentially mimics latent cooling from a dry microburst in which most, if not all, of the hydrometeors melt, evaporate, and/or sublimate before reaching the ground. The cooling source is stationary as is common in the downburst literature . compare this method with a translating source and conclude that both are viable methods for downburst simulations.

3 Results

A brief analysis of the evening transition simulation (which provides the initial conditions for the downburst simulations) is presented in Sect. 3.1, followed by a detailed analysis of the downburst cases in Sect. 3.2. The analysis performed herein is from the lowest 2 km of the simulation domain in order to limit any influence from the damping layer.

## 3.1 ET simulation

The evening transition simulation produces hourly restart files to be used as the initial conditions for each of the downburst simulations. The potential temperature and wind velocity profiles for each case are shown in Fig. 3. As can be seen, both the C1 and C2 temperature profiles (red and yellow lines, respectively) are unconditionally unstable throughout the boundary layer with the instability reducing to zero by case N (gray line). Even though the surface temperature is decreasing between the C1 and C2 cases, the prescribed temperature is still larger than that of the mixed layer. The warmer surface combined with the warming from entrainment (mixing of the warm air above the boundary layer into the mixed layer) results in a continual warming in the mixed layer between C1 and C2. As the simulation progresses, a surface-based stable layer develops by S1 and deepens to S2 (green and blue lines, respectively). The mixed layer temperature between the C2 and N cases continues to subtly warm. In previous ET studies, it has been shown that entrainment can persist due to residual convection after the surface heating has stopped . During the generation of the stable layer, the average wind speed throughout the residual layer (remnant of the mixed layer) increases along with the deepening of shear below roughly 250 m. This low-level stable layer is estimated to be as deep as 200 m.

The vertical sensible heat flux profiles are normalized relative to the surface sensible heat flux of the C1 case. It can be seen here that over time the amount of vertical sensible heat flux near the surface and within the mixed layer decreases to zero by the N case and becoming negative after. The decrease of vertical sensible heat flux throughout the boundary layer occurs from the bottom up as is consistent with the literature . The ET is defined as the period in which the boundary layer becomes approximately neutral near the surface and achieves a vertical sensible heat flux of zero at the lowest model level. The negative portion of vertical sensible heat flux above roughly 1.5 km is caused by entrainment. The height at which the vertical sensible heat flux is most negative is often used to define the daytime boundary layer height. Entrainment acts to increase the boundary layer height most notably between C1 and C2.

Figure 4 shows a vertical cross section of the w-component velocity field for the C1–5x_5y (top row), N–5x_0y (middle row), and S2–0x_5y (bottom row) cases along with average profiles of the u- and v-component winds in the right column. These cross sections are taken from the location of maximum vertical velocity in order to get a sense for the strongest of the updrafts within the domain. As can be seen in the C1–5x_5y simulation, strong thermals are present within the model domain in which vertical velocities reach over 6 m s−1. As the surface heating decreases, the strength of the thermals becomes weaker. However, by the time the atmosphere reaches a near-neutral regime, remnants of these thermals are still prevalent throughout the domain. After 2 more hours of stabilization, these remnants have largely dissipated as shown in the S2–0x_5y panel.

Analyzing the average profiles of the u- and v-component winds in Fig. 4, it is clear to see the increase in v-component wind speeds as stability increases. In the stable cases, a sharp increase in the v-component winds below roughly 100 m is seen due to the Coriolis force causing the winds to veer with height within the SBL (Stull1988).

Figure 4Vertical cross sections of vertical velocity and average profiles of the u- and v-component winds for the C1–5x_5y (a, b), N–5x_0y (c, d), and S2–0x_5y (e, f) cases at the start of the downburst runs. Cross sections are taken along the east–west axis at the y location where the maximum vertical velocity occurs. Filled contours show vertical velocity (m s−1) with arrows representing the uw wind field. The domain average u- and v-component wind speed profiles are shown in the right column in black and red, respectively.

## 3.2 Downburst simulations

The downburst simulations are each run for 15 min. After about 13 min, the outflow reaches the domain boundary in each simulation. For this reason, only data from the vertical plane at x=6.0 km are analyzed for the full 15 min as the boundaries do not influence these results. Between the different downburst simulations, only the initial and boundary conditions are changed. Surface temperature is decreased, as within the ET simulation, for the full downburst duration. For generalization purposes, the ensemble mean for several of the analysis fields is presented here. However, in order to gain insight into the individual downbursts, a characteristic simulation is chosen from each case for certain analyses. Downburst simulation results are presented by referring to time in minutes after the case initiation, denoted by timeburst. The hours into the ET simulation at which the downburst cases are initiated can be seen in the schematic presented in Fig. 2.

### 3.2.1 Velocity fields

In each of the downburst simulations, a diverging outflow pattern in the horizontal wind fields is generated as shown in Fig. 5. The initial (top row) and mature-to-dissipating (bottom row) stages of the downbursts are shown for the C1–5x_5y (left column), N–5x_0y (center column), and S2–0x_5y (right column) cases. These horizontal cross sections are taken at around 100 m above ground level, a typical value for the hub height of a commercial wind turbine. The initial stages of the downbursts show large swaths of areas with horizontal winds greater than 20 m s−1 (denoted by black arrows), mostly confined to regions downwind of the downburst (i.e., to the right of the downburst center). At this stage, the C1 and N cases appear to generate generally stronger horizontal winds than the stable, S2, case. However, below 100 m, the wind speeds for all cases increase (not shown), suggesting that the wind speeds in the S2 case are simply confined to lower heights than the other cases. As the outflow evolves, by timeburst=10.25 min, the S2 case has fully developed a large, strong horizontal outflow region while the convective case has begun to dissipate. It can be seen that the ambient winds in the C1 case have much more variability than the N and S2 cases, which effectively deforms and disorganizes the outflow.

Figure 5Horizontal cross sections at 98.13 m for the C1–5x_5y (a, d), N–5x_0y (b, e), and S2–0x_5y (c, f) cases at timeburst=7.5 min (a, b, c) and 10.25 min (d, e, f). Filled contours show the temperature (K) with arrows representing the horizontal wind field at this level. The locations with wind speeds above 20 m s−1 are shaded in black, while locations with wind speeds below this threshold are shaded in gray. The north–south-oriented line denotes the location at which a vertical slice is recorded at every time step used to generate the time series in Fig. 7.

The large regions of high winds extending generally in the north–south direction in Fig. 5 are organized by the ring vortex. This feature can be seen near the vertical dashed line in Fig. 6 for each of the presented cases. The ring vortex increases the wind speed beneath it; the center of this ring vortex occurs at increasingly higher elevations as stability increases. The depth of the head of the outflow is also seen to increase with increasing stability due to the interactions of the ambient winds with the outflow – a similar result to what has been reported based on RKW theory (see , for details). This theory shows how low-level shear can interact with outflow to generate stronger, more vertically upright updrafts from the counteracting vortices from the outflow and the ambient environment. Interestingly, a similar result is also reported in the simulations by , where, by only introducing a surface-based temperature inversion, the depth of the outflow and the height of the ring vortex increase to equal the depth of the stable layer. In the present environment, both an increase in low-level shear and a surface-based temperature inversion are considered and a qualitatively similar trend is observed.

Figure 6Vertical cross sections along the east–west axis at the center of the domain for the C1–5x_5y (a, b), N–5x_0y (c, d), and S2–0x_5y (e, f) cases at timeburst=7.5 min. Filled contours show temperature (K) with arrows representing the uw wind field. In panels (b, d, f) are the horizontal velocity and vertical velocity profiles (black and blue, respectively) for each case at the dashed line in the vertical cross section (of a, c, e).

The vertical wind shear generated from the development of the ring vortex can easily be seen in the vertical profiles of horizontal (black) and vertical (blue) winds in Fig. 6 (right panels). These profiles are taken at the center of the domain in the y direction and at the location of the maximum wind speed in the x direction. In each case, the maximum wind speed occurs behind the center of the ring vortex. The associated upward motions (see the S2–0x_5y panel) and downward motions (see the C1–5x_5y and N–5x_0y panels) can be seen in the vertical velocity profile. These motions are confined mostly to the lowest 500 m. The vertical structure in the horizontal winds in case C1–5x_5y shows an increasing horizontal wind from the height of the ring vortex down to the surface. Cases N–5x_0y and S2–0x_5y, however, show a vertical structure below around 250 m that is quite complex. The wind speeds decrease from the lowest level to around 150 m, then sharply increase again before quickly decreasing to ambient wind speeds at 500 m. The strongest horizontal wind speeds occur at the lowest model level in these cases, but the secondary peak above this appears to be associated with the temperature gradient generated by the warm air entraining into the ring vortex. It should be noted that these complex wind patterns are occurring at heights that would impact typical commercial wind turbines.

To get an idea of the temporal structure at a single point during the passage of the downburst, Fig. 7 shows the magnitude of velocity (M; black line) and the individual components of the wind field (u, v, and w) in red, green, and blue, respectively, at ymax. Here, ymax is defined as the location along the vertical cross sections at which the maximum horizontal wind speed occurs at 98.13 m above the ground over the full 15 min duration. This location will change from case to case as the maximum wind speeds along this cross section do not always happen at the same location. The time series are shown at 98.13 m for direct comparison with Fig. 5 for each of the simulations in cases C1 (panel a), N (panel b), and S2 (panel c). Each of the ensemble members are shown to highlight the extent of the deviation between runs. By studying the vertical velocity time series (blue line) for each case, the time between peak-positive and peak-negative vertical wind speeds (indicative of the ring vortex passage) is seen to be as short as 20 s to as long as about 1 min. Generally, this time between these positive and negative peak values increases as stability increases. This is due to the associated increased spatial extent of the ring vortex or due to a decrease in the speed at which it propagates (, found that a low-level temperature inversion decreased the propagation speed of the outflow). Each case also shows the maximum wind speed occurring in between the maximum updraft and maximum downdraft, consistent with the passage of the ring vortex.

In the C1 simulations, the vertical velocity and lateral velocity components are quite low relative to the other simulations. This is because ymax is located closer to the center of the domain and because a weaker ring vortex forms in these convective simulations. In the neutral simulations, the ymax locations are split between north of center and south of center (indicated by the positive and negative peaks, respectively, in the v-component wind speeds), hinting at a lack in preferential location of occurrence of the maximum wind speed. In contrast, in the S2 simulations, all of the ymax locations are north of center, where the outflow propagation direction is normal to the direction of the low-level wind shear vector. A similar result was found in a numerical case study by of a dry, pulsating microburst event. In the current model, the low-level wind shear is generated by the Coriolis effect on the low-level stable layer (Stull1988). This is consistent with the added ambient shear in the stable cases that bolsters the ring vortex and, thus, helps to increase horizontal wind speeds at this location. Here, we also see that the peak horizontal wind speed reaches the vertical cross section at x=6.0 km earlier in the C1 simulations and later in the S2 simulations. Although there are differences in the propagation speed from case to case, the differences in timing here are due to the circular nature of the downburst resulting in the ramp reaching locations along the vertical slice at different times. The location of ymax changes in each case, with the S2 cases showing a preference to locations along the slice further from the center of the domain, which results in the wind ramp occurring at a later time than the C1 and N cases. Lastly, the additional stability in the S2 cases allows the wind field to recover to pre-outflow values more rapidly; this recovery is thus a function of the stability as well as the location of ymax.

The ensemble mean of the domain-maximum horizontal wind speeds at each height with time is presented using filled contours in Fig. 8. Open contours of the ensemble mean of the maximum downdraft (black) and maximum updraft (dotted magenta) are also included in this figure in order to deduce the state of the downburst. Several generalizations can be made about the structure of the maximum wind speeds for each of the simulations. First, the initial signal of the downburst comes from a rapid increase in intensity of the downdraft. Then, horizontal wind speeds near the surface begin to increase; this is followed by a strengthening of the updraft wind speeds between around 100 and 300 m. The peak wind speed is generally reached just after the updraft band develops with the exception of the C1 case, where the two appear to occur simultaneously in the ensemble-averaged output. Finally, as the updraft band begins to vertically expand, the horizontal outflow decreases. This happens at different times and rates for each case. The collocation of the updraft and downdraft bands is due to the ring vortex. When these bands expand and taper off, it is indicative of a ring vortex that has become disorganized and begun to dissipate.

Figure 7Time series of the velocity components at the location (x=6 km, y=ymax, z=98.13 m) for the C1 (a), N (b), and S2 (c) cases at the 6.0 km cross section (red dashed line in Fig. 5).

Figure 8A time–height plot in the lowest 500 m of the ensemble average of maximum horizontal velocity for the C1, C2, N, S1, and S2 cases going from panels (a–e). Contoured (in black) are the ensemble averages of minimum vertical velocity starting from 10 m s−1 and drawn at 5 m s−1 intervals and (in dotted magenta) the ensemble averages of maximum vertical velocity starting from positive 10 m s−1 and drawn at 2.5 m s−1 intervals.

Inspecting C1, it is clear that the strength of the downdraft is weaker than the other simulations. This is due to the interaction of convective thermals and increased turbulent motions as the downburst descends through the column (see the top-left panel in Fig. 4). The impact of this interaction can be seen in Fig. 6, where the downdraft (between roughly 3.0 and 4.5 km in the west–east direction) is noticeably more disorganized in the C1 case but much more coherent in the N and S2 cases. By timeburst=11 min in Fig. 8, the downdrafts are no longer below 10 m s−1 and the updrafts begin to ascend farther from the surface. This shows the demise of the ring vortex and coincides with the rapid weakening of the near-surface winds.

As the stability increases, it can be seen that the maximum downdraft increases and that it also develops at a faster rate. Further, the initial depth of the strong horizontal winds produced from the outflow is contained closer to the surface with increasing stability, indicating an increase in outflow-generated shear across the low levels of the atmosphere. Decay of the strong updrafts and downdrafts occurs at later times as stability increases, with case S2 showing the first signs of decay at timeburst=12 min.

Several downburst modeling studies have attempted to find a relationship between the maximum outflow wind speed (Ustorm) to maximum downdraft (wmin) by calculating the ratio of Ustorm to wmin . showed that it was difficult to deduce any universal relationship between Ustorm and wmin in the brief study on the low-level stability. However, in his model, microphysics were being utilized and, thus, many more variables came into play in this scenario which makes deducing any relationships more complex. In this study, we attempt to determine relationships between this ratio and stability. Due to the peak wind speeds occurring so close to the surface, the vertical component is almost negligible; thus, in our computation of Ustorm we do not include the vertical velocity component .

Figure 9 shows plots of the Ustorm, wmin, and the ratio of Ustorm to wmin in the top, middle, and bottom rows, respectively, for the different simulations: C1 (red), C2 (yellow), N (gray), S1 (green), and S2 (blue). These quantities are plotted against the bulk Richardson number (Stull1988) at the lowest model level and averaged over the first 3 min of the simulation to deduce their relationships with stability. In studying the maximum outflow wind speed, a subtle and almost insignificant increase can be seen with increasing stability. The spread of the values tends to decrease as stability increases as well, owing to the heterogeneity of the convective simulations transitioning to the more homogeneous, stable regime. When considering only the ensemble mean values, as shown in Table 1, an increase with stability can be generally seen, although it is not an entirely monotonic increase. The maximum wind speeds of 35–38 m s−1 are consistent with strong observed downbursts: 25–30 m s−1 in , 32 m s−1 (with theorized maxima in the F3 range of 70–92 m s−1) in , and 67 m s−1 in . Further, other observed modeling studies have generated similar wind speed maxima of 38 m s−1 , 35 m s−1 , 57 m s−1 , 35–65 m s−1 , 24–32 m s−1 , and 47 m s−1 .

In contrast, wmin is clearly strengthened with increasing stability as can be seen in Fig. 9 and Table 1. As previously mentioned, this is most likely attributed to the decrease in turbulence which would act to impede the downburst as it descends. In tracking the height at which the maximum downdraft occurs for each ensemble member, Table 1 shows a somewhat unclear relationship between the ensemble mean maximum downdraft and ensemble mean of the heights at which this downdraft occurs. Here, we can see that the higher downdraft wind speeds are occurring at lower heights. Intuitively, one might expect the stable surface layer to impede the progress of the downburst at lower heights and force the peaks to occur at higher levels. The opposite is seen in the cases herein, likely because the stable layer developed in the ET simulation is too shallow to impede the downdraft.

Finally, comparing the ratio of Ustorm to the magnitude of wmin in Fig. 9, we notice what appears to be a converging pattern to a value of roughly 1.3 as stability increases. The spread of values decreases significantly from the C1 cases to the two stable cases. Overall, the range of values of this ratio is in line with what other downburst simulations have produced ( showed values ranging from 0.8 to 2.4, although this was while varying microphysics; simulations by produced a value of 1.58 in neutral conditions; and produced a value of 1.34 in neutral conditions). It is not quite clear how universal this ratio is, as the maximum downdraft is clearly shown to depend on the ambient environment and the maximum outflow will depend on the environment as well as on variables such as surface roughness.

Figure 9Variations of Ustorm (a), wmin (b), and the ratio between the two (c) for each case – C1 (red), C2 (yellow), N (gray), S1 (green), and S2 (blue) – with the average bulk Richardson number at the first model level over the first 3 min of simulation. Circles represent the 0x_0y cases, the right-pointing triangles represent the 5x_0y cases, the upward-pointing triangles represent the 0x_5y cases, and the diamonds represent the 5x_5y cases. The ensemble mean is denoted by an ”x” for each case.

As downbursts develop and mature, the maximum wind speeds move with the ring vortex farther away from the downburst center. To show this, the downburst center is predicted as the location of maximum divergence over a roughly 1 km diameter area in both the x and y directions and is calculated every 15 s. This process occasionally results in large jumps in the predicted downburst center location between model time steps; thus, in order to ameliorate the prediction, a linear regression is performed for the predicted centers between timeburst=6 and 10.5 min and extrapolated to all times. Next, the maximum wind speeds at the lowest model level are recorded for each simulation in bins of 100 m expanding radially from the downburst center. In this way, we are able to track how the downburst expands and how the velocity field changes with radial distance from the center and with time as shown in Fig. 10. Here, only wind speeds to the right of the downburst center (downstream) are considered for the C1 (top row), N (middle row), and S2 (bottom row) cases with each ensemble member (columns 1 through 4) and the ensemble average (far right column) shown. It is clear that in each of the C1 simulations, the outflow begins to weaken earlier on in the simulations than for the neutral and S2 cases. C1–0x_5y, for example, appears to deteriorate just after reaching the surface. The length of time over which the outflow persists appears to be related to the ambient stability. The ensemble mean for the S2 case shows what appears to be a rather constant-intensity wind speed of around 30 m s−1 that persists past 12 min while the other cases show considerable weakening by this time. The propagation speed of the downbursts also appears to change with stability. In the S2 case, the peak wind speeds initially move away from the downburst center at a much quicker rate than for the other cases. However, after a minute or so, this propagation away from the center begins to slow to a pace similar to that of the C1 ensemble mean. , being the only study in which a stable regime has been tested that we are aware of, showed that a low-level temperature inversion acts to weaken the outflow wind speed, slow the propagation rate, and decrease the peak downdraft. In the simulations herein, the opposite occurs (see Table 1). This could be due to several factors: first, the depth of the stable layer is much shallower in these simulations (, considered an artificial temperature inversion through a depth of 500 and 1000 m); second, the inclusion of low-level shear in these simulations appears to play a significant role in maintaining the ring vortex and, thus, generating a more persistent outflow; and third, utilizes a RANS model, whereas an LES model is utilized herein.

Upon studying the ensemble average for each case, it is clear that the C1 case increases to its peak velocity much quicker than the N and S2 cases. For each case, the time from which divergence at the lowest model level first increases past 0.5 times the average environmental surface divergence, $\mathrm{\nabla }\cdot {U}_{\mathrm{sfc}}=\mathrm{1.5}\mathrm{\nabla }\cdot {U}_{{\mathrm{sfc}}_{\mathrm{0}}}$, to the time at which the maximum wind speed occurs, tmax, is calculated and presented in Table 1 under tramp. The variable, tramp, shows that the convective cases reach peak velocity quicker than in the neutral and stable cases, perhaps because the turbulence disorganizes the outflow more rapidly. However, it is interesting to note that the neutral case takes the longest time to reach peak velocity. On average, the S2 cases reach their peak velocity in less time than the S1 cases. We speculate that this is due to the ring vortex developing quicker with increased shear or potentially due to the additional negative buoyancy ingested from the surface-based stable layer.

Figure 10Variation with time of the horizontal wind speed (m s−1) at the lowest model level at binned radii to the right of the downburst center for cases C1 (a), N (b), and S2 (c). Each case is presented in the first four columns while the ensemble mean is shown in the right column.

Table 1Ensemble-averaged maximum event horizontal wind speed, ensemble-averaged maximum event downdraft, and the ratio of those two for each case, along with the ensemble average of the time from first sign of divergence at the surface ($\mathrm{\nabla }\cdot {U}_{\mathrm{sfc}}=\mathrm{1.5}\mathrm{\nabla }\cdot {U}_{{\mathrm{sfc}}_{\mathrm{0}}}$) to the time of maximum surface wind speed.

### 3.2.2 Ensemble-averaged variances

Throughout each simulation, domain-averaged profiles of several resolved variances, ${\mathit{\sigma }}_{{u}_{i}}^{\mathrm{2}}\left(t,z\right)$, ${\mathit{\sigma }}_{{v}_{i}}^{\mathrm{2}}\left(t,z\right)$, and ${\mathit{\sigma }}_{{w}_{i}}^{\mathrm{2}}\left(t,z\right)$, are calculated and output every second for each ensemble member, i, in order to analyze how the downburst wind fields modify the environment. Note that with increased resolution, it is expected that the resolved variances will increase in the S1 and S2 cases. The resolution achieved in this model setup is adequate for convective and neutral simulations. Next, the ensemble averages, $〈{\mathit{\sigma }}_{{u}_{\mathrm{Ens}}}^{\mathrm{2}}〉\left(t,z\right)$, $〈{\mathit{\sigma }}_{{v}_{\mathrm{Ens}}}^{\mathrm{2}}〉\left(t,z\right)$, and $〈{\mathit{\sigma }}_{{w}_{\mathrm{Ens}}}^{\mathrm{2}}〉\left(t,z\right)$, are computed for each case to get a generalized result. The profiles of maximum variance for the background (dotted) and the downburst (solid) are reported in Fig. 11. In terms of the environment for the maximum u- and v-component ensemble-averaged variances, the magnitude of these variances is seen to decrease with increasing stability. However, with the passage of the downburst, the peak variances occur near the surface and increase in magnitude as stability increases (note that due to the profiles being first domain-averaged, the variance generated by the downburst and the ambient environment are both included in these values). Both the u- and v-component variances return very close to their ambient values by around 400 m and only truly begin to deviate and increase below 200 m. The right panel shows the maximum of the ensemble-averaged vertical velocity variance, where a much more interesting feature is seen to develop. In the most convective case (C1), the maximum vertical velocity variance appears to increase while generally retaining the shape from the ambient profile. However, as the environment becomes more stable, a nose-like profile begins to form. First, noticeable in C2, the nose increases in value (but not in height) to case N. As the stable layer develops, the peak begins to increase in height (but not much in value) from the N to the S2 case. Above this nose, the maximum begins to decrease as the environment becomes more stable. As opposed to the variances from the other two components of the wind field, the vertical velocity variance is the lowest at the surface, as one would expect, but grows significantly even with the influence of the ambient environment in the domain-averaged profile and reaches its peak value between around 160 and 225 m. The combination of these variances being so large and their being so highly sheared within the lowest 200 m of the atmosphere further emphasizes the dangers of downburst winds to structures such as wind turbines.

Figure 11Profiles of the maximum u, v, and w variance of the ensemble mean in panels a, b, c), respectively, for each case. In each plot, for a given height, the maximum ensemble variance is computed over a specific time interval. In the case of the environment (dotted lines), the first 3 min of the output are considered, whereas, in the case of the downbursts, the first 13 min are utilized for the analysis.

Figure 12The same as Fig. 8 but for vertical velocity variance.

In order to determine the cause of the nose-like structure in the maximum of the ensemble-averaged vertical velocity variance, Fig. 12 shows the variation with time of the ensemble mean of the vertical velocity variance profiles for each case. As in Fig. 8, open contours of negative (positive) vertical velocity in black (dotted magenta) are included for reference. At the time of the strongest downdraft, the ensemble-averaged vertical velocity variance is large for the convective cases but much weaker for the stable cases. This is due partly to the increased ambient vertical velocity variance in the convective cases, as can be seen in minutes 1–5 of the simulations, as well as to the increased mixing from the cool downburst and warm thermals. As the outflow develops in each case, the vertical velocity variance shows a clear area of maximum variance coincident with the areas of large positive and negative vertical velocity. It is at this height that the nose-like feature exists and is due to the formation of the ring vortex. Further, it can be seen that the convective and neutral cases have heights of the area of maximum values that are around 160 to 175 m, while the S1 and S2 cases indicate that these heights are 200 and 225 m, respectively. This also appears to be around the same heights as the top of the surface-based temperature inversion and low-level shear layers shown in Fig. 3, thus confirming results from , where the height of the ring vortex is equivalent to that of the stable layer.

### 3.2.3 Coherent turbulent kinetic energy

Coherent, or organized, turbulent structures have been shown to increase structural loads and fatigue in wind turbines and have factored into decision-making for all aspects of the wind energy community from turbine design to siting and operation . and define coherent turbulent kinetic energy, or CTKE, as a fluid dynamic parameter which describes both spatially and temporally organized motions in a turbulent field. While the primary focus for calculating CTKE has been for low-level jets and Kelvin–Helmholtz waves, here we compute the parameter from the organized turbulent motions of the downburst and associated ring vortex. The calculation of CTKE as defined in is as follows:

$\begin{array}{}\text{(4)}& \mathrm{CTKE}=\mathrm{0.5}\sqrt{〈{u}^{\prime }{w}^{\prime }{〉}^{\mathrm{2}}+〈{u}^{\prime }{v}^{\prime }{〉}^{\mathrm{2}}+〈{v}^{\prime }{w}^{\prime }{〉}^{\mathrm{2}}},\end{array}$

where $〈{u}^{\prime }{w}^{\prime }〉$, $〈{u}^{\prime }{v}^{\prime }〉$, and $〈{v}^{\prime }{w}^{\prime }〉$ are the domain averages of the kinematic momentum flux components. As an extension to the more conventional turbulent kinetic energy (TKE), CTKE effectively represents the amount of fluxes that are associated with organized structures. For example, in a completely random (homogeneous and isotropic) turbulent field, CTKE would be zero while TKE would be finite.

The total fluxes necessary to compute CTKE are output as domain-averaged profiles every second of the simulation. Figure 13 shows the now familiar time–height plots with positive and negative vertical velocity contours for the ensemble-averaged value of CTKE for each case. Here we see that the convective cases generate the highest values of CTKE just as the downburst forms and strengthens. A trace of higher values of CTKE can also be seen at higher levels just after the maximum downdrafts occur and descending to where the ring vortex develops (most prominent in the neutral and stable cases). Interestingly, the simulations with the most well-defined ring vortices (S1 and S2) show the lowest values of CTKE at the levels in which the ring vortex exists. In each of the cases, the levels with the largest amounts of CTKE are in the lowest 150 m. The convective cases have large amounts of CTKE through deeper levels; in contrast, case S1 shows a large amount of CTKE focused below 50 m and decreasing quickly above.

Figure 13The same as Fig. 8 but for coherent turbulent kinetic energy (CTKE).

### 3.2.4 Wavelet spectral analysis

In order to quantify the energy at different scales, wavelet spectral analysis of the u-component wind field at 98.13 m is performed for each ensemble member of each case. The wavelet spectrum is computed from the time series data output every 1 s for each y location using the Daubechies-5 (db5) wavelet. Sensitivity to the wavelet was performed with the Symmlet-8 wavelet and the results showed very little dependence on the wavelet type (not shown). Due to the curvature of the outflow winds, the wind ramp does not occur for the selected vertical slice at the same time for all y. Thus, the wavelet spectra are averaged along y between 4.5 and 5.5 km where the outflow reaches the vertical slice at roughly the same time. Further, at these points, as the outflow is almost directly to the east of the downburst center, the wind field is largely dominated by the u component. Figure 14 shows the resulting ensemble average of the wavelet power spectra for each case. The white portions of the figures are the areas inside of the “cone of influence”, the region in which edge effects become important . The non-stationary character of the turbulence associated with the u-component wind field is clear to see in each case. As would be expected, the ambient energy (from timeburst=2–6 min) is higher for the convective cases and lower for the stable cases. In general, the lowest frequencies or small wavenumbers contain the peak in the wavelet spectra. At the time of the first impact of downbursts, energy increases by a factor of 10 or more across all the scales almost instantly. After this time, energy slowly declines across all frequencies. The convective cases resolve the highest amounts of energy at low frequencies compared to the other cases. As stability increases, the amount of energy resolved generally decreases; however, case S1 produces a fair amount more energy than the N and S2 cases. This same pattern is seen when studying CTKE (Fig. 13).

Figure 14Ensemble-averaged wavelet power spectrum of u-component velocity (m2 s−1) at 98.13 m using the Daubechies-5 wavelet for the C1, C2, N, S1, and S2 cases from top to bottom, respectively.

4 Summary and conclusions

In this study, a pseudo-spectral LES code is utilized to simulate several idealized downbursts during the ET. The ET is first simulated by spinning up a convective boundary layer and then linearly decreasing the surface temperature such that the boundary layer passes through a neutral regime and ultimately achieves a stable regime. The idealized downbursts are generated through a three-dimensional cooling source located over the top of the boundary layer to create a pocket of negatively buoyant air mimicking the latent cooling of evaporation, melting, and sublimation during a downburst. Downburst simulations are initialized separately within the various PBL regimes, allowing for the effects of stability to be analyzed. Additionally, several instances are run for each stability regime by modifying the initial conditions in order to yield more generalized results. This is necessary due to the random locations of thermals in the convective boundary layer (and to a lesser extent, the neutral and stable boundary layers), which causes significant variation in the downburst winds. Analyses of these results allow for the following conclusions to be drawn:

• As seen with observed thunderstorm winds (see Fig. 1), the ensemble-averaged maximum wind speed remains fairly constant through each stability regime. However, the stable cases produce the most consistent and strongest outflow winds when compared to the convective and neutral cases. The consistency appears to be due to the increased homogeneity in the stable wind field and lack of ambient turbulence, while the increased severity is attributed to either a stronger ring vortex due to increased low-level shear, increased negative buoyancy generated from the vertical advection of the surface-based stable layer by the ring vortex, or a combination of the two.

• The maximum downdraft wind appears to show a direct positive correlation with increasing stability.

• The stronger ring vortex and associated stronger winds persist for a longer duration in the stable cases than in the convective and neutral cases due to the lack of turbulence to disorganize this feature. Further, the height of the ring vortex center increases with increasing stability, up to the height of the stable layer with the depth of the downburst head (based on temperature) becoming deeper in the stable cases.

• Maximum wind speeds are realized directly downstream from the center for the convective cases and north of the center for the stable cases; it appears that wind speeds reach their maxima where the outflow propagation direction is normal to the direction of the low-level wind shear vector. In the stable cases, the direction of the wind turns more southwesterly at the lowest levels, thus aligning the ambient wind shear vector with the northeast quadrant of the outflow winds.

• Calculations of CTKE show generally higher amounts of energy in the convective cases as the downburst first reaches the surface and spreads laterally. Wavelet analysis shows that this sudden increase in energy occurs across all scales as the downburst passes and then slowly begins to decline.

At the time of publication, a follow-up paper is currently in progress in which the output from these downburst simulations will be utilized as input into the FAST model. This work will aim to quantify the relationship downburst winds in various ambient stability regimes with the structural loads and stresses on commercial wind turbines.

Future work, motivated by the present study, includes a deeper investigation into the effects of stability on the dynamics of the downburst winds. Specifically, there is interest in isolating the effects of turbulence, low-level shear, and the surface-based temperature inversion in order to assess which boundary layer characteristics have the greatest impact on the downburst flow. Further, investigations into the relationship of outflow wind intensity and depth of the stable layer are planned; simulations by have shown that a deep enough stable layer can inhibit downburst winds and even prevent them from reaching the ground entirely. These studies will also allow the relationship between the depth of the stable layer and strength of the downburst in producing a heat burst to be determined. It is also of interest to investigate the accuracy of the current modeling framework for downbursts in various stability regimes. While it is reasonable to assume that the outflow winds from downbursts may encounter various stability regimes while advancing away from the downburst center, it is unclear to what extent the environment directly underneath the downburst is turbulent during the descent. Thus, future LES studies of the downburst-producing thunderstorm utilizing microphysics parameterizations are necessary to increase the realism of the simulations and to determine the representativeness of these findings.

Data availability
Data availability.

The simulated data (several terabytes in size) are freely available for any non-commercial research usage. They are archived in network-attached storage systems. Please contact the corresponding author for access.

Competing interests
Competing interests.

The authors declare that they have no conflict of interest.

Acknowledgements
Acknowledgements.

This work was supported by the National Science Foundation (NSF) under grant nos. CBET-1336760 and CBET-1336304.

Edited by: Joachim Peinke
Reviewed by: two anonymous referees

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