The Inn Valley
Our location of interest is the Inn Valley in Austria, a mostly west–east oriented major valley in the eastern Alps. The Inn River flows through the valley surrounded by mountains with peak heights between 2000 and 3000 m and side valleys of different size. The Inn Valley and its surroundings have been subject of various observational and numerical studies, exploring gap flows (Mayr et al. 2007), foehn winds (Gohm et al. 2004; Gohm and Mayr 2004), air pollution scenarios (Gohm et al. 2009; Schicker and Seibert 2009; Schnitzhofer et al. 2009), and the daytime up-valley flow, which is quite robust to synoptic forcing (Vergeiner and Dreiseitl 1987; Zängl 2004, 2009). A strong thermally-driven circulation in the Inn Valley also influences the velocity field at larger scales in the Bavarian foreland known as Alpine pumping. Observations and regional climate simulations suggest that this phenomenon occurs on average around 60 days per year (Graf et al. 2016).
Observations
The so-called “Innsbruck Box” (i-Box) project is designed as a “reference box” to explore the ABL structure and exchange processes in complex terrain (Rotach et al. 2017). The i-Box observations consist of state-of-the-art measurement systems and instruments such as turbulence-flux towers (Stiperski and Rotach 2016) located in the Inn Valley, a scintillometer, a Doppler wind lidar, and a HATPRO temperature and humidity profiler (Massaro et al. 2015), located in the city of Innsbruck, and automatic weather stations in an extended mesonet.
We mainly focus on observations from the core sites (turbulence flux towers) located some 30 km east of the city of Innsbruck. Figure 1 shows the spatial distribution of the i-Box stations. The locations of the stations are representative for characteristic surfaces in complex terrain, such as the valley floor, and both south- and north-facing slopes. Since most of the flux towers are operational since the year 2013, this is a unique data pool of high-quality turbulence measurements, especially for locations in complex terrain, and offer the possibility to evaluate high-resolution NWP models in detail.
All the data analysis and quality control procedures of the measurement data are described in Stiperski and Rotach (2016). More specifically, the fluxes were calculated for 30-min averaging periods and double rotation was used to align the data into the slope-normal coordinate system. Prior to calculation the data were filtered using a recursive filter with a time constant of 200 s. Turbulence dissipation was estimated from the power spectra of the two horizontal velocity components using the spectral method (Piper and Lundquist 2004). For this purpose the inertial subrange was detected as the region where the power spectrum had a \(-\,5/3\) slope. The 4/3 ratio between the power spectra of the horizontal velocity components was used as a quality criterion.
Numerical Model
We perform numerical simulations with the COSMO model (version 5.0). The COSMO model is a limited area model that was originally developed for high-resolution, convection-resolving, operational NWP by the Deutscher Wetterdienst (Baldauf et al. 2011). Multiple national weather services have joined the consortium with their own versions of the model. Besides operational versions, simulations were also successfully performed for research purposes over mountainous terrain for, e.g., model evaluation studies with ABL observations (Collaud Coen et al. 2014), idealized model inter-comparison studies (Schmidli et al. 2010; Buzzi et al. 2011), and parametrization testing (Anurose and Subrahamanyam 2015; Panosetti et al. 2016). In our work, we focus on the evaluation of the operational set-up of MeteoSwiss with \(\Delta x=1.1\,\hbox {km}\).
Set-up
The model solves the non-hydrostatic, fully compressible hydro-thermodynamical equations on an Arakawa C-grid. A third-order Runge–Kutta scheme is employed for time integration (Klemp and Wilhelmson 1978; Wicker and Skamarock 2002) and a fifth-order advection scheme is used for temperature, pressure, and velocity, while a second-order advection scheme is applied for moist quantities (Bott 1989). Radiation is parametrized via a \(\delta \) two-stream radiation scheme (Ritter and Geleyn 1992), which includes a full cloud-radiation feedback. The effects of topographic shading are implemented in the model code following Müller and Scherer (2005), while a cumulus parametrization scheme after Tiedtke (1989) is switched on for shallow convection. The COSMO model uses the multi-layer soil model TERRA-ML consisting of eight soil levels with eight soil types. In the operational set-up, turbulence is parametrized with a 1.5-order closure following Mellor and Yamada (1982) with a prognostic equation for TKE. The model also offers an option to include horizontal shear production with a Smagorinsky-type turbulence treatment. More details can be found below.
Our model set-up is similar to the operational COSMO-1 set-up of MeteoSwiss (de Morsier et al. 2012). The model uses two domains: the outer domain with a horizontal grid spacing of \(\Delta x =6.6\,\hbox {km}\) (COSMO-7) spans Europe and is driven by ECMWF IFS-HRES data.Footnote 1 The inner domain, which is slightly smaller than the operational domain by MeteoSwiss, consists of \(800 \times 600\) grid points, spans the main Alpine range (Fig. 2), and uses the data from the outer domain as boundary fields. The horizontal grid spacing is \(\Delta x = 1.1\,\hbox {km}\) with a timestep of \(\Delta t=10\,\hbox {s}\), with 80 vertical levels employed in terrain-following smooth level vertical coordinates (Schär et al. 2002; Leuenberger et al. 2010). The lowest model half-level is located at a height of 10 m above ground and 40 vertical levels lie below 3000 m, which is roughly the height of the surrounding topography. The model topography (Fig. 2) is derived from the Advanced Spaceborne Thermal Emission and Reflection Radiometer (ASTER) Global Digital Elevation MapFootnote 2 and resolves the Alps and their major valleys, including the Inn Valley, adequately for daytime up-valley flows (Zängl 2004, 2009). Closer comparisons with the high-resolution ASTER topography suggest that mountaintops are smoothed and that smaller side valleys are not well-resolved (Rotach et al. 2017, their Fig. 1), which may pose a challenge for the simulation of smaller-scale circulation patterns. External parameters for land-use and soil data on a horizontal grid spacing of \(\Delta x= 1.1\,\hbox {km}\) are derived from the Harmonized World Soil Database (HWDFootnote 3).
Turbulence Parametrization Evaluation
We evaluate the model’s turbulence parametrization by means of case studies. The model is either initialized at 0000 UTC for daytime or 1200 UTC for night-time simulations and runs for 24 h; thus the first few hours of the simulations are considered as spin-up time and not considered in the analysis. We focus on days when the thermally-driven circulation dominates the ABL structure in the Inn Valley. Favorable weather patterns for these flows are cloud-free days, a strong up-valley flow in the Inn Valley (wind speed \(> 4\,\hbox {m}\, \hbox {s}^{-1}\)) and the corresponding wind direction (\(\approx 090^{\circ }\) at the valley-floor station). During the consecutive cloud-free nights, drainage flows are present at the valley floor and on the slopes. Overall, we choose eight cases from the i-Box data pool that satisfy our criteria (simulation initiation time in brackets): 11 June 2014 (1200 UTC), 16 September 2014 (0000 UTC), 1 July 2015 (0000 and 1200 UTC), 28 August 2015 (1200 UTC), 29 August 2015 (0000 UTC), and 8 September 2015 (0000 and 1200 UTC). For all days, we conduct the simulations with both a 1D turbulence parametrization and a hybrid turbulence parametrization (see below).
The main quantity investigated is the TKE and its contributing budget terms, since it provides direct information about the status of the ABL (Stull 1988). When comparing the model to the measurements (Table 1), one must keep in mind that, (i) the height above mean sea level (a.m.s.l.) between model terrain and real terrain is different, (ii) the lowest model half-level is located at 10 m above ground level (a.g.l.), while the sensor heights of the flux towers are different, and (iii) the type of location (i.e., south-facing slope, valley floor) of the closest grid point of the model may diverge from the actual location, especially when the terrain representation is not appropriate.
Table 1 shows the height and slope angle of the i-Box stations and their representation in the model. The station on the valley floor (CS-VF0) is well-represented in terms of height a.m.s.l., however, in the model, the valley floor is slightly inclined. The stations with the optimun local terrain representation are on two slopes directly facing each other, namely CS-SF8 and CS-NF10. The other two stations on the slopes have either a too-steep slope angle in the model (CS-SF1) or a too-flat slope (CS-NF27). The type of location does not differ much, e.g., a north-facing slope is a north-facing slope in both observations and model.
Table 1 A detailed overview of the i-Box stations (see Fig. 1 for their locations) taken into account, and their representation in the numerical model: \(\alpha \) indicates the slope angle
Since one single grid point of the model might not be representative of the ABL structure in that part of the valley, we employ a so-called grid-point ensemble: first, the closest model grid point to an i-Box station is determined via horizontal Euclidean distance. As a next step, we include the eight nearest grid points and calculate from this small nine-member ensemble the mean, median, 75th and 90th percentiles. Clearly, the question of how many members the grid-point ensemble should contain is related to the scale of the problem. Based on test simulations the scale of horizontal inhomogeneity is on the order of several 100 m–2 km while the scale of the topography is several km. The choice of nine ensemble members therefore is a compromise between these two constraints.
Observed TKE
When comparing the full TKE budget equation to that of the model, we have to consider the differences between modelled TKE budget terms and observed TKE budget terms. The observed TKE, \(\bar{e}\), is directly calculated from the velocity variances observed at the i-Box stations
$$\begin{aligned} \bar{e}= \frac{1}{2} (\overline{u'^2}+\overline{v'^2}+\overline{w'^2}). \end{aligned}$$
(1)
Generally, the full TKE budget equation can be written as follows (Stull 1988)
$$\begin{aligned} \underbrace{\frac{ \partial \bar{e}}{ \partial t}}_\text {local tendency}+\underbrace{\overline{U_j}\frac{ \partial \overline{e}}{ \partial x_j}}_\text {advection}= & {} \underbrace{{\delta _{i3} \frac{g}{\overline{\theta _v}}(\overline{u_i'\theta _v'})} }_{\begin{array}{c} \text {buoyancy}\\ \text {production/consumption} \end{array}} -\underbrace{{\overline{u_i'u_j'}\frac{ \partial \overline{U_i}}{ \partial x_j}}}_{\begin{array}{c} \text {shear}\\ \text {production} \end{array}} \nonumber \\&-\underbrace{\frac{ \partial (\overline{u_j'e})}{ \partial x_j}}_\text {turbulent transport }- \underbrace{\frac{1}{\overline{\rho }} \frac{ \partial (\overline{u_i'p'})}{ \partial x_i}}_\text {pressure correlation}-\underbrace{{\varepsilon }}_\text {dissipation} \end{aligned}$$
(2)
where capital letters with overbars denote mean quantities, while small letters with primes refer to turbulent fluctuations; \(\bar{e}\) is TKE, U is the mean wind speed, g is the acceleration due to gravity, \(\theta _v\) is virtual potential temperature, \(\rho \) is air density, and p is pressure. On the left-hand side (l.h.s.) are the local TKE tendency and advection with the mean flow, while on the right-hand side (r.h.s.) we find the thermally-driven buoyancy production/consumption term, the mechanical shear production term, the turbulent transport, the pressure correlation term, which mainly serves as TKE redistribution, and the TKE dissipation rate \(\varepsilon \), which is always a sink for TKE.
1D Turbulence Parametrization
While the full TKE equation is three-dimensional, the model’s turbulence closure considers only vertical turbulent processes. Note that this is the case for virtually all operational NWP settings—even when the model is operated at comparably high resolution and over complex terrain. In the first set of simulations, we therefore use the model’s 1.5-order turbulence closure at a 2.5-hierarchy level of Mellor and Yamada (1982), and refer to it as “turb_1D scheme”. The model solves the prognostic equation for the TKE making use of an auxiliary variable q defined by \(q=\sqrt{2\bar{e}}\) or vice versa \(\bar{e}={q^2}/2\),
$$\begin{aligned} \underbrace{\frac{D}{Dt}\left( \frac{q^2}{2}\right) }_\text {tendency}= & {} -\underbrace{K_H \frac{g}{\theta } \frac{\partial \theta }{\partial z}}_{\begin{array}{c} \text {buoyancy} \\ \text {production/consumption} \end{array}} + \underbrace{ K_M\left[ \left( \frac{ \partial U}{ \partial z}\right) ^2+\left( \frac{ \partial V}{ \partial z}\right) ^2\right] }_\text {vertical shear production} \nonumber \\&+\underbrace{\frac{1}{\overline{\rho }}\frac{ \partial }{ \partial z}\left[ \alpha _{\text {tke}}\overline{\rho }\lambda _l q \frac{ \partial }{ \partial z}\left( \frac{q^2}{2}\right) \right] }_\text {vertical turbulent transport}-\underbrace{\frac{q^3}{B_1\lambda _l}}_\text {dissipation}. \end{aligned}$$
(3)
The term on the l.h.s. is the tendency of TKE. Note that this term can be split into a local tendency part (\(\frac{\partial }{\partial t} \frac{q^2}{2}\)) and an advection part. However, the advection is only invoked in the hybrid turbulence parametrization as described in the follow-up section. The first two terms on the r.h.s. are the buoyancy production/consumption term and the vertical shear production term, where \(K_H\) and \(K_M\) are the turbulent diffusivity and conductivity, respectively. For more details on the calculation of stability functions and constants see Appendix B-1 of Buzzi (2008) and Buzzi et al. (2011). In the vertical turbulent transport term, \(\alpha _{\text {tke}}\) is a parameter from the parametrization scheme, and the turbulence length scale \(\lambda _l\) is calculated after Blackadar (1962),
$$\begin{aligned} \lambda _l=\lambda ^{\infty }_{l}\frac{\kappa (z+z_0)}{\kappa (z+z_0)+\lambda ^{\infty }_{l}}. \end{aligned}$$
(4)
Here, \(\lambda ^{\infty }_{l}\) is an asymptotic length scale, \(z_0\) is the aerodynamic roughness length, \(\kappa \) is the von Kármán constant, and z is the respective height above ground. The Blackadar length scale is a widely-used approach and was developed for larger scales, though it should be noted that it might perform poorly in convective conditions when eddies reach the size of the ABL height (Chrobok et al. 1992).
We note here that the pressure correlation term (Eq. 2) plays a similar role as the turbulent transport term in redistributing TKE. Since it is usually considered small it is not explicitly modelled in the operational turb_1D scheme. In complex terrain, however, taking the pressure correlation term to be small may be a dangerous assumption. The dissipation follows Kolmogorov’s law, while \(B_1\) is a constant model parameter after Mellor and Yamada (1982). Note that this parametrization of the dissipation rate implies isotropic turbulence, which is often not the case in shear-generated turbulence in complex terrain. The COSMO model has also an option to include subgrid-scale orographic drag. However, at our horizontal grid spacing, the larger-scale terrain is already adequately resolved, therefore this effect is considered as small and is consequently not invoked; however, it could play a role in the stable ABL (Steeneveld et al. 2009).
The model’s surface transfer scheme uses a diagnostic TKE equation (Buzzi 2008, Appendix B-2). The surface transfer layer is defined as the layer between the surface and the lowest model level, where the transfer coefficients are computed, and consists of three sublayers: a laminar sublayer, a turbulent roughness sublayer, and a constant-flux (Prandtl) sublayer. The roughness sublayer reaches from the surface, where the turbulent length scale \(l=\lambda /\kappa \) is zero, to a level where \(l=z_0\). The Prandtl sublayer above extends from l up to the first model level, therefore a discrimination between model variables at the surface predicted by the soil model and atmospheric values at l is possible. The fluxes are formulated in resistance form and interpolation schemes are used for the calculation of the transport resistances. The necessary boundary-layer profiles are derived from the dimensionless coefficients \(K_M\) and \(K_H\) of the Mellor–Yamada framework. This scheme therefore avoids the empirical functions of Monin-Obukhov similarity theory, which are in general not applicable in complex terrain (Stiperski and Rotach 2016). This surface transfer scheme is employed in the operational set-ups of the COSMO model (Baldauf et al. 2011), and also in the regional climate model version, COSMO-CLM (Langhans et al. 2013; Leutwyler et al. 2016).
Hybrid Turbulence Parametrization
Extensions to the turb_1D scheme are available in the COSMO model (Blahak 2015): the advection of \(q=\sqrt{2 \bar{e}}\) is computed together with the other advective tendencies of model variables and added in the follow-up timestep to the TKE budget. Recall that in the model code, the TKE equation is solved for \(q=\sqrt{2 \bar{e}}\), because q is an important quantity in the Mellor–Yamada framework. Therefore, the advected quantity is q, not directly the TKE, \(\bar{e}\). Horizontal diffusion is calculated in terrain-following coordinates.
The vertical shear production term in the TKE equation can be extended to three dimensions, thereby also considering horizontal shear production in the TKE budget. This is achieved by calculating the horizontal contributions to shear production with a Smagorinsky closure (Smagorinsky 1963; Langhans et al. 2012). The shear production of TKE due to horizontal gradients is determined as follows and then added to the model TKE equation,
$$\begin{aligned} \frac{\partial }{\partial t}\left( \frac{q^2}{2}\right) _{{Shear}_{hor}}=(c \Delta x)^2 \left[ \left( \frac{ \partial U}{ \partial x}\right) ^2+\left( \frac{ \partial V}{ \partial y}\right) ^2+\frac{1}{2}\left( \frac{ \partial U}{ \partial y}+\frac{ \partial V}{ \partial x}\right) ^2\right] ^{\frac{3}{2}}, \end{aligned}$$
(5)
where c is the dimensionless Smagorinsky constant with a value of 0.2, and \(\Delta x\) is the horizontal grid spacing.
With these two additional contributions to the TKE equation, we have a “hybrid” set-up (“turb_hybrid” scheme hereafter): the vertical contributions to the TKE is calculated with the Mellor–Yamada framework, while the horizontal contributions to TKE are calculated with a method usually used for large-eddy simulations (LES). The COSMO model also offers a fully 3D Smagorinsky-Lilly scheme for LES, which is not suitable for our horizontal grid spacing (Honnert and Masson 2014; Cuxart 2015).
Comparison to Observations
It is challenging to compare all the terms of the TKE budget to the available observations, therefore we provide an overview of our methodology in the following paragraphs.
We have observations of TKE itself, the buoyancy production/consumption term (estimated with the observed sensible heat flux), and the TKE dissipation rate. Therefore, these quantities can be directly compared to the model results from the lowest model level. The observed vertical turbulent transport can be approximated for stations with TKE observations at two or more levels, which is the case at the valley floor station (CS-VF0),
$$\begin{aligned} \frac{ \partial (\overline{u_3'e})}{ \partial x_3}\approx \frac{\Delta (\overline{w'e})}{\Delta z} \end{aligned}$$
(6)
where the values for the difference are taken from the lowest (4 m) and highest (17 m) level of the measurement tower. Similarly, vertical shear production can be estimated from flux towers with two or more levels of mean wind observations (CS-VF0, CS-NF27, and CS-SF8), and can be compared with the model’s vertical shear production term. We estimate four horizontal terms of the shear production (Eq. 2) at the valley floor station (CS-VF0) with the observations from the south-facing slope station that is located at a similar altitude (CS-SF8, Fig. 1),
$$\begin{aligned}&\overline{u'u'}\frac{ \partial \overline{U}}{ \partial x}+ \overline{u'v'}\frac{ \partial \overline{U}}{ \partial y}+ \overline{u'v'}\frac{ \partial \overline{V}}{ \partial x}+ \overline{v'v'}\frac{ \partial \overline{V}}{ \partial y} \nonumber \\&\quad \approx \overline{u'u'} \frac{\Delta \overline{U}}{\Delta x}+\overline{u'v'} \frac{\Delta \overline{U}}{\Delta y}+\overline{u'v'} \frac{\Delta \overline{V}}{\Delta x}+\overline{v'v'} \frac{\Delta \overline{V}}{\Delta y} \end{aligned}$$
(7)
where the velocity components \(\overline{U}\) and \(\overline{V}\) are rotated back into the Cartesian coordinate system, and \(\Delta x=2.19\, \hbox {km}\) and \(\Delta y=2.25\, \hbox {km}\), respectively. Here the fluxes are taken from the CS-VF0 station, noting that there are no observations of mean TKE advection.