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Stability influences on interscale transport of turbulent kinetic energy and Reynolds shear stress in atmospheric boundary layers interacting with a tall vegetation canopy

Published online by Cambridge University Press:  29 June 2021

Laurent Perret*
Affiliation:
LHEEA, UMR CNRS 6598, Centrale de Nantes, 44230 Nantes, France Institut de Recherche en Sciences et Techniques de la Ville (IRSTV), FR CNRS 2488 Nantes, France
Edward G. Patton
Affiliation:
National Center for Atmospheric Research, Boulder, CO 80305, USA
*
†Email address for correspondence: laurent.perret@ec-nantes.fr

Abstract

High-resolution data from the large-eddy simulation of the atmospheric boundary layer (ABL) over a vegetation canopy are used to investigate the interaction between the most energetic large-scale structures from the ABL and the smaller scales from the near-canopy region. First, evidence of amplitude modulation (AM) involving the three velocity components is demonstrated. A multi-scale analysis of the transport equation of both the turbulent kinetic energy (TKE) and Reynolds shear stress (RSS) is then performed using a multi-level filtering procedure. It is found that, on average, in the investigated region, large scales are a source of TKE for the small scales (e.g. forward scatter of TKE) through nonlinear interscale transfer ($T_r^L$) with a maximum at canopy top while they are a sink via turbulent transport ($T_t^L$). Close to the canopy, the small-scale RSS transport behaves the same while, above the roughness sublayer, $T_r^L$ and $T_t^L$ switch roles showing the existence of RSS backscatter. The standard deviation of the transfer terms shows that there are intense instantaneous forward and backscatter of both TKE and RSS via all the transfer terms. It is therefore demonstrated that there is a two-way coupling between the ABL and the near-canopy scales, the well-known top-down mechanism through TKE transfer being complemented by a bottom-up feedback through RSS transfer. This analysis is extended to several stability regimes, confirming the above conclusions and showing the increasing role of the large-scale wall-normal component in AM and TKE or RSS transfers when the flow becomes buoyancy driven.

Information

Type
JFM Papers
Copyright
© The Author(s), 2021. Published by Cambridge University Press
Figure 0

Figure 1. Schematic diagram of the dual-hairpin eddy formation from Patton & Finnigan (2013) (adapted from Finnigan et al.2009).

Figure 1

Table 1. Main characteristic parameters of each simulation, including the geostrophic wind $U_g$ ($V_g=0$), the friction velocity $u_*$, the buoyancy flux $\langle w' \theta _v' \rangle$, the ABL depth $z_i$ where, these $z_i$ values are calculated using the ’maximum vertical gradient method’ (Sullivan et al.1998) using virtual potential temperature as the scalar, the Obukhov length $L$, the vorticity thickness at canopy top $\delta _\omega$, the convective velocity scale $w_*$, the mixed velocity scale $w_m$ and the potential temperature scale $\theta _*$ (adapted from Patton et al.2016).

Figure 2

Figure 2. Multi-level decomposition of the variable $u$ shown in spectral space in the case of sharp cutoff filters, depicting interactions between $\delta u^{(n)}=\bar {u}^{(n+1)}-\bar {u}^{(n)}$ and: (A) the larger scales $u^{(n+1)}$ via the term ${\mathcal {L}}_{ij}^{(n+1)}$, (B) a spectral band $\delta u^{(m)}$ at some smaller scale ($m< n$) via the term $\sum _{k=m+1}^{n-1}({\mathcal {G}}_{k+1}^{(n+1)}-{\mathcal {G}}_{k+1}^{(n)}){\mathcal {L}}_{ij}^{(k)}$, (C) all the scales $u''$ smaller than the LES-filter scale $\bar {\varDelta }^{(m)}$ via the term $({\mathcal {G}}_{m+1}^{(n+1)}-{\mathcal {G}}_{k+1}^{(n)})T_{ij}^{(m)}$ (adapted from Sagaut et al.2013). The definition and derivation of the terms ${\mathcal {L}}_{ij}^{(n)}$ and $T_{ij}^{(m)}$ can be found in Appendix A.2.

Figure 3

Figure 3. Four-level decomposition shown in spectral space depicting the budget terms for $(\xi ^S)^2$ the (small) canopy-scale TKE, as listed in table 2. The terms representing the spatial transport of $(\xi ^S)^2$ by $u^S$ and $u^L$ (labelled $T_t^S$ and $T_t^L$, respectively), are shown with dashed line circles, the production of $(\xi ^S)^2$ by the mean flow $P^M$ and the interscale transfer of TKE between $u^S$ and $u^L$ (labelled $T_r^L$) are shown with solid line arrows, the influence of canopy drag $D_r$ is shown with a dotted line arrow and the production of $(\xi ^S)^2$ by buoyancy (labelled $B^S$) is shown with a zig-zag arrow. Vertical dashed lines sketch the different cutoff filters involved in the four-level decomposition: the LES filter, the cutoff filter employed to separate the resolved scales $u^L$ and $u^S$ and the horizontal averaging operation.

Figure 4

Table 2. Budget terms for $(\xi ^S)^2= \frac {1}{2} [(u^S)^2+(v^S)^2+(w^S)^2]$ the small-scale TKE investigated in the present study. Equivalent terms for the small-scale RSS are calculated as well (see Appendix D.2).

Figure 5

Figure 4. Horizontal ensemble-averaged wall-normal profiles of $(a)$ horizontal wind speed $\langle u_h \rangle = (\langle u \rangle ^2 +\langle v\rangle ^2)^{1/2}$, $(b)$ temperature $\langle \theta \rangle$, $(c)$ resolved heat flux $\langle w^\prime \theta ^\prime \rangle /(w_m \theta _m)$, $(d)$ horizontal velocity variance $(\langle {u^\prime }^2 \rangle +\langle {v^\prime }^2\rangle )/w_m^2$, $(e)$ vertical velocity variance $\langle {w^\prime }^2 \rangle /w_m^2$ and $(f)$ RSS $\langle u^\prime w^\prime \rangle /w_m^2$ for all the cases (the WU case is shown in blue dashed lines).

Figure 6

Figure 5. Instantaneous fluctuations normalized by $w_m$ of (left) $u$, (centre) $v$ and (right) $w$ in the $x$–$y$ plane at ($a$,$b$,$c$) $z/h=10$, ($d$,$e$,$f$) $z/h=5$ and ($g$,$h$,$i$) $z/h=1$ for the WU case. Panels ($j$,$k$,$l$) are close up views of the centre of the velocity field at $z/h=1$ corresponding to the black squares shown in ($g$,$h$,$i$).

Figure 7

Figure 6. Pre-multiplied spectra of the three velocity components plotted as a function of the wall-normal distance $z$ and (left) the streamwise wavelength $\lambda _x$ and (right) the transverse wavelength $\lambda _y$ (normalized by $z_i$ or $h$) (WU case). Pre-multiplied spectra normalized by $w_m^2$ of $u, v$ and $w$ are shown in ($a$,$b$), ($c$,$d$) and ($e$,$f$), respectively. The vertical dashed line shows the cutoff wavelength chosen for scale separation. The red dashed line indicates the location of the local maximum of the spectra. Oblique dotted blacked lines correspond to trends $\lambda ^m \propto z^2$ in ($a$,$c$,$d$) and $\lambda ^m \propto z$ in ($b$,$e$,$f$) of the most energetic canopy scales in the region $1< z/h<5$. Spectra are scaled up by a factor of $10^4$ for clarity. For clarity, 20 contours are distributed logarithmically between 0.025 and the maximum of each spectrum. The horizontal dark-green long-dashed line corresponds to canopy top.

Figure 8

Table 3. Streamwise and spanwise wavelengths $\lambda _x^m$ and $\lambda _y^m$ corresponding to the most energetic scales of the three velocity components in the different regions of the flow, normalized by the canopy height $h$ or the boundary-layer depth $z_i$.

Figure 9

Figure 7. Pre-multiplied cospectra plotted as a function of the wall-normal distance $z$ and the (left) streamwise wavelength $\lambda _x$ and (right) the transverse wavelength $\lambda _y$ (normalized by $z_i$ or $h$) (WU case). The negative of the pre-multiplied cospectra of $w$ and $u$ (e.g. vertical momentum flux) normalized by $w_m^2$ are shown in ($a$,$b$) and pre-multiplied cospectra of $w$ and $\theta$ (e.g. vertical heat flux) normalized by $w_m\theta _m$ are shown in ($c$,$d$). The vertical dashed line shows the cutoff wavelength retained for scale separation. The red dashed line indicates the location of the local maximum of the spectra. Cospectra are scaled up by a factor of $10^4$ for clarity. For clarity, 20 contours are distributed logarithmically between 0.025 and the absolute maximum of each cospectra. The horizontal dark-green long-dashed line corresponds to canopy top.

Figure 10

Figure 8. Instantaneous velocity signals showing AM at $z/h=1$. $(a)$ instantaneous fluctuations $u^\prime$ of the streamwise velocity component, $(b)$ large-scale component of $u^\prime$, $(c)$ fluctuations of the low-pass-filtered envelope $E^L({u_i^\prime }^S)$ of the small-scale velocity components (solid line) ${u^\prime }^S$, (dashed line) ${v^\prime }^S$ and (dotted line) ${w^\prime }^S$, $(d)$ (solid black line) small-scale TKE $(\xi ^S)^2$ and (dotted red line) low-pass filtered envelope of $(\xi ^S)^2$. See text for the definition of the employed low-pass filter. (WU case).

Figure 11

Figure 9. The AM coefficients of the three small-scale velocity components ($\blacksquare$, red) $u^S$, ($\bullet$, blue) $v^S$, ($\blacktriangle$, green) $w^S$ and ($\blacktriangledown$, black) the corresponding TKE $(\xi ^S)^2$ by $(a)$ the large-scale streamwise velocity component $u^L$, $(b)$ the large-scale spanwise velocity component $v^L$ and $(c)$ the large-scale wall-normal velocity component $w^L$ (WU case). The beige shaded area corresponds to the canopy region.

Figure 12

Figure 10. Wall-normal evolution of ($a$,$c$) the mean and $(b,\!d)$ standard deviation of the interscale transfer terms ($\blacksquare$, red) $T_t^S$, ($\bullet$, blue) $T_t^L$, ($\triangle$, pink) $P^M$, ($\blacktriangledown$, orange) $T_r^L$, ($\diamond$, green) $D_r$ and (solid black line) $B^S$ (as in table 2) for ($a$,$b$) the small-scale TKE $(\xi ^S)^2$ and ($c$,$d$) RSS $-u^Sw^S$ (WU case). Positive values indicate a gain for the small scales.

Figure 13

Figure 11. The AM coefficients $AM(u_i^L,\xi ^S)$ between the small-scale TKE $(\xi ^S)^2$ and the large-scale $(a)$ streamwise velocity component $u^L$, $(b)$ spanwise velocity component $v^L$ and $(c)$ wall-normal velocity component $w^L$, for each atmospheric stability cases listed in table 1.

Figure 14

Figure 12. Wall-normal profiles of the mean interscale transfer terms ($\blacksquare$, red) $T_t^S$, ($\bullet$, blue) $T_t^L$, ($\triangle$, pink) $P^M$, ($\blacktriangledown$, orange) $T_r^L$, ($\diamond$, green) $D_r$ and (black solid line) $B^S$ for the small-scale TKE $(\xi ^S)^2$, for all the atmospheric stability cases listed in table 1. Positive values indicate a gain for the small scales. Please note that the $x$-axis range changes between panels.

Figure 15

Figure 13. Wall-normal profiles of the mean interscale transfer terms ($\blacksquare$, red) $T_t^S$, ($\bullet$, blue) $T_t^L$, ($\triangle$, pink) $P^M$, ($\blacktriangledown$, orange) $T_r^L$ and ($\diamond$, green) $D_r$ and (black solid line) $B^S$ for the small-scale RSS $-u^Sw^S$, for all the atmospheric stability cases listed in table 1. Positive values indicate a gain for the small scales. Please note that the $x$-axis range changes between panels.

Figure 16

Figure 14. Mean interscale transfer term $T_r^L$ normalized by the sum of the shear and buoyancy production terms $P^M+B^S$ for $(a)$ small-scale TKE $(\xi ^S)^2$, and $(b)$ the small-scale RSS $-u^S w^S$, as a function of the wall-normal distance, for the five stability regimes. See corresponding text for the definition of each term.

Figure 17

Figure 15. Contribution of the terms involving horizontal gradients of the large-scale velocity field to the TKE interscale transfer term $T_r^L$ as a function of the wall-normal distance, for the five stability regimes. See corresponding text for the definition of each term.

Figure 18

Figure 16. Confidence interval of the horizontal ensemble-averaged wall-normal profiles of $(a)$ horizontal wind speed $\langle u_h \rangle = (\langle u \rangle ^2 +\langle v\rangle ^2)^{1/2}$, $(b)$ temperature $\langle \theta \rangle$, $(c)$ resolved heat flux $\langle w^\prime \theta ^\prime \rangle /(w_m \theta _m)$, $(d)$ horizontal velocity variance $(\langle {u^\prime }^2 \rangle +\langle {v^\prime }^2\rangle )/w_m^2$, $(e)$ vertical velocity variance $\langle {w^\prime }^2 \rangle /w_m^2$ and $(f)$ Reynolds shear stress $\langle u^\prime w^\prime \rangle /w_m^2$ for the WU case. The black solid lines show the present statistics computed over $N_v=4$ LES three-dimensional volumes. Blue shaded areas represent a 95 % confidence bound of the statistics of the WU case due to statistical error. The beige shaded area shows the region occupied by the canopy.

Figure 19

Figure 17. Confidence interval of the mean interscale transfer terms $T_t^S, T_t^L, P^M, T_r^L, D_r$ and $B_S$ of ($a$,$b$,$c$,$d$,$e$,$f$) the small-scale TKE $(\xi ^S)^2$ and ($g$,$h$,$i$,$j$,$k$,$l$) the small-scale RSS $-u^S w^S$, for the WU case. The black dashed lines and the shaded areas show the 75 % and 95 % confidence bounds, respectively. The solid lines show the average values obtained from the $N_v=4$ LES volumes, as shown in figure 10($a$,$c$).