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  <front>
    <journal-meta>
<journal-id journal-id-type="publisher">ACP</journal-id>
<journal-title-group>
<journal-title>Atmospheric Chemistry and Physics</journal-title>
<abbrev-journal-title abbrev-type="publisher">ACP</abbrev-journal-title>
<abbrev-journal-title abbrev-type="nlm-ta">Atmos. Chem. Phys.</abbrev-journal-title>
</journal-title-group>
<issn pub-type="epub">1680-7324</issn>
<publisher><publisher-name>Copernicus GmbH</publisher-name>
<publisher-loc>Göttingen, Germany</publisher-loc>
</publisher>
</journal-meta>

    <article-meta>
      <article-id pub-id-type="doi">10.5194/acp-15-10071-2015</article-id><title-group><article-title>Turbulence vertical structure of the boundary layer during the afternoon transition</article-title>
      </title-group><?xmltex \runningtitle{Turbulence vertical structure of the boundary layer during the
afternoon transition}?><?xmltex \runningauthor{C.~Darbieu et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1">
          <name><surname>Darbieu</surname><given-names>C.</given-names></name>
          <email>darc@aero.obs-mip.fr</email>
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Lohou</surname><given-names>F.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-4374-0127</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Lothon</surname><given-names>M.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff2">
          <name><surname>Vilà-Guerau de Arellano</surname><given-names>J.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0003-0342-9171</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff3">
          <name><surname>Couvreux</surname><given-names>F.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Durand</surname><given-names>P.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff4 aff5">
          <name><surname>Pino</surname><given-names>D.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-4512-0175</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff6">
          <name><surname>Patton</surname><given-names>E. G.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-5431-9541</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1 aff7">
          <name><surname>Nilsson</surname><given-names>E.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff4">
          <name><surname>Blay-Carreras</surname><given-names>E.</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff8">
          <name><surname>Gioli</surname><given-names>B.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0001-7631-2623</ext-link></contrib>
        <aff id="aff1"><label>1</label><institution>Laboratoire d'Aérologie, Toulouse, CNRS UMR 5560, Université de
Toulouse, Toulouse, France</institution>
        </aff>
        <aff id="aff2"><label>2</label><institution>Meteorology and Air Quality Section,
Wageningen University, Wageningen, the Netherlands</institution>
        </aff>
        <aff id="aff3"><label>3</label><institution>CNRM-GAME
(Météo-France and CNRS), Toulouse, France</institution>
        </aff>
        <aff id="aff4"><label>4</label><institution>Department of
Applied Physics, Universitat Politècnica de Catalunya, BarcelonaTech,
Barcelona, Spain</institution>
        </aff>
        <aff id="aff5"><label>5</label><institution>Institute of Space Studies of Catalonia
(IEEC-UPC), Barcelona, Spain</institution>
        </aff>
        <aff id="aff6"><label>6</label><institution>National Center for Atmospheric
Research, Boulder, Colorado, USA</institution>
        </aff>
        <aff id="aff7"><label>7</label><institution>Uppsala University, Uppsala,
Sweden</institution>
        </aff>
        <aff id="aff8"><label>8</label><institution>Institute of Biometeorology, National Research Council
(IBIMET-CNR), Florence, Italy</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">C. Darbieu (darc@aero.obs-mip.fr)</corresp></author-notes><pub-date><day>9</day><month>September</month><year>2015</year></pub-date>
      
      <volume>15</volume>
      <issue>17</issue>
      <fpage>10071</fpage><lpage>10086</lpage>
      <history>
        <date date-type="received"><day>7</day><month>November</month><year>2014</year></date>
           <date date-type="rev-request"><day>22</day><month>December</month><year>2014</year></date>
           <date date-type="rev-recd"><day>24</day><month>July</month><year>2015</year></date>
           <date date-type="accepted"><day>24</day><month>July</month><year>2015</year></date>
      </history>
      <permissions>
<license license-type="open-access">
<license-p>This work is licensed under a Creative Commons Attribution 3.0 Unported License. To view a copy of this license, visit <ext-link ext-link-type="uri" xlink:href="http://creativecommons.org/licenses/by/3.0/">http://creativecommons.org/licenses/by/3.0/</ext-link></license-p>
</license>
</permissions><self-uri xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015.html">This article is available from https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015.html</self-uri>
<self-uri xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015.pdf">The full text article is available as a PDF file from https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015.pdf</self-uri>


      <abstract>
    <p>We investigate the decay of planetary boundary layer (PBL) turbulence in the
afternoon, from the time the surface buoyancy flux starts to decrease until
sunset. Dense observations of mean and turbulent parameters were acquired
during the Boundary Layer Late Afternoon and Sunset Turbulence (BLLAST) field
experiment by several meteorological surface stations, sounding balloons,
radars, lidars and two aircraft during the afternoon transition. We analysed a case study based on some of
these observations and large-eddy simulation (LES) data focusing on the
turbulent vertical structure throughout the afternoon transition.</p>
    <p>The decay of turbulence is quantified through the temporal and vertical
evolution of (1) the turbulence kinetic energy (TKE), (2) the characteristic
length scales of turbulence and (3) the shape of the turbulence spectra. A
spectral analysis of LES data, airborne and surface measurements is performed
in order to characterize the variation in the turbulent decay with height and
study the distribution of turbulence over eddy size.</p>
    <p>This study highlights the LES ability to reproduce the turbulence evolution
throughout the afternoon. LESs and observations agree that the afternoon
transition can be divided in two phases: (1) a first phase during which the
TKE decays at a low rate, with no significant change in turbulence
characteristics, and (2) a second phase characterized by a larger TKE decay
rate and a change in spectral shape, implying an evolution of eddy size
distribution and energy cascade from low to high wave number.</p>
    <p>The changes observed either in TKE decay (during the first phase) or in the
vertical wind spectra shape (during the second phase of the afternoon
transition) occur first in the upper region of the PBL. The higher within the
PBL, the stronger the spectra shape changes.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <title>Introduction</title>
      <p>The transition from a well-mixed convective boundary layer to a residual
layer overlying a stable nocturnal layer raises several issues
<xref ref-type="bibr" rid="bib1.bibx34" id="paren.1"/>, which remain difficult to address from both modelling and
observational perspectives. The well-mixed convective boundary layer with
fully developed turbulence is mainly forced by buoyancy. The afternoon
decrease in the surface buoyancy flux leads to the decay of the turbulence
kinetic energy (TKE) and a change in the structure of the turbulence, which
shows more anisotropy and intermittency. It is important to better understand
the processes involved, as they can influence the dispersion of tracers in
the atmosphere <xref ref-type="bibr" rid="bib1.bibx53 bib1.bibx6 bib1.bibx5 bib1.bibx52" id="paren.2"><named-content content-type="pre">e.g.</named-content></xref> and the development of the nocturnal and daytime boundary layers
of the following days <xref ref-type="bibr" rid="bib1.bibx2" id="paren.3"/>.</p>
      <p>Turbulence decay has been studied with laboratory experiments
<xref ref-type="bibr" rid="bib1.bibx38 bib1.bibx7" id="paren.4"><named-content content-type="pre">e.g.</named-content></xref>, theoretical models <xref ref-type="bibr" rid="bib1.bibx15" id="paren.5"/>,
numerical studies with large-eddy simulations (LESs) <xref ref-type="bibr" rid="bib1.bibx40 bib1.bibx49 bib1.bibx44" id="paren.6"><named-content content-type="pre">e.g.</named-content></xref> and observations <xref ref-type="bibr" rid="bib1.bibx13 bib1.bibx17 bib1.bibx3 bib1.bibx12" id="paren.7"><named-content content-type="pre">e.g.</named-content></xref>. In all of these studies, the decay was mainly
related to the decrease in the surface buoyancy flux but with complexity
gained with shear-driven boundary layers <xref ref-type="bibr" rid="bib1.bibx43 bib1.bibx16" id="paren.8"/>,
which slow the decay. Using LESs, <xref ref-type="bibr" rid="bib1.bibx40" id="text.9"/> considered a sudden shut-off
of surface heat flux and found that turbulence decay occurred within a period
of the order of the convective timescale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mo>*</mml:mo></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi>w</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula>, where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the
planetary boundary layer (PBL) depth and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>w</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula> is the convective velocity
scale <xref ref-type="bibr" rid="bib1.bibx9" id="paren.10"/>. However, different results were obtained if a
slower decrease in the forcing surface buoyancy flux is considered with an
external timescale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">f</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> <xref ref-type="bibr" rid="bib1.bibx49 bib1.bibx44 bib1.bibx45 bib1.bibx39" id="paren.11"/>. If <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">f</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is large relative to <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula>, the
turbulence can adjust to the forcing change, in quasi-equilibrium, as noted
by <xref ref-type="bibr" rid="bib1.bibx7" id="text.12"/>. This is the case in the mid-afternoon PBL, when
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula> is around 10 or 15 min and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">f</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is around 2 or 3 h.
<xref ref-type="bibr" rid="bib1.bibx49" id="text.13"/> found that the TKE decay scales with <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">f</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi>t</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula>,
with <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula> estimated at the start of the decay. But in late afternoon and
around sunset, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula> starts to increase significantly (until the definition
of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>w</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula> becomes questionable at zero buoyancy
flux), and turbulence may not be able to adjust to the external change.
Consequently, an extensive description of the turbulence structure is needed
to better understand this decay process in the PBL.</p>
      <p>The evolution of the turbulence length scales across the afternoon transition
has not been addressed extensively, but several studies can be found that
show diverging results. Considering eddy lifetime, or the “turn over”
timescale, one may state that smaller eddies will decay earlier than larger
eddies <xref ref-type="bibr" rid="bib1.bibx8" id="paren.14"/>. This is one explanation given by
<xref ref-type="bibr" rid="bib1.bibx49" id="text.15"/>, from an LES study, for the increase in the characteristic
length scale of the vertical velocity found in the mixed (then residual)
layer of the LES. In the surface layer, one may expect the length scales to
decrease, as inferred by <xref ref-type="bibr" rid="bib1.bibx22" id="text.16"/> from the study of surface-layer
spectra evolution with stability during the Kansas experiment. On the basis
of tethered-balloon observations, <xref ref-type="bibr" rid="bib1.bibx17" id="text.17"/> showed that the peak of the
vertical velocity spectrum shifts to smaller length scales in the surface
layer during the evening transition. Finally, <xref ref-type="bibr" rid="bib1.bibx40" id="text.18"/> and
<xref ref-type="bibr" rid="bib1.bibx43" id="text.19"/> found that the length scale of the maximum spectral energy
of the vertical velocity remained constant during the decay process. By using
a theoretical model of the TKE spectrum and LES, <xref ref-type="bibr" rid="bib1.bibx16" id="text.20"/> have
also found that the spectral peak remains at approximatively the same
wavelength when shear is strong enough to prevent the spectral peak of
vertical velocity from shifting towards shorter wavelengths. For other
meteorological variables, such as the horizontal wind components, temperature
and moisture, <xref ref-type="bibr" rid="bib1.bibx43" id="text.21"/> have shown that the characteristic length
scales increase with time.</p>
      <p>The evolution of the turbulence scales remains unclear and only partly
understood. It must be thoroughly investigated whether the scales in the
mixed, and afterward residual, layer really increase or not. Considering the
time response and equilibrium aspect mentioned above, and the possible
decoupling with height between the stabilizing surface layer and the
overlying residual layer, it is also important to consider the vertical
structure of turbulence decay, i.e. the evolution of turbulence and scales as
a function of height. Except for <xref ref-type="bibr" rid="bib1.bibx16" id="text.22"/>, the numerical studies
quoted above <xref ref-type="bibr" rid="bib1.bibx49 bib1.bibx43" id="paren.23"><named-content content-type="pre">e.g.</named-content></xref> considered TKE to be
integrated over the entire PBL depth, and observations of the turbulence
decay were, most of the time, made at surface <xref ref-type="bibr" rid="bib1.bibx39" id="paren.24"/>. Only a few
observational studies considered the vertical structure of the turbulence's
afternoon decay (<xref ref-type="bibr" rid="bib1.bibx17 bib1.bibx13" id="altparen.25"/>, on the afternoon-decaying PBL).</p>
      <p>Here we investigate the evolution of the turbulence spectra and scales from
surface to PBL top during the afternoon
transition (AT) based on the BLLAST (Boundary Layer Late Afternoon and Sunset
Turbulence) data set, collected during the summer of 2011 <xref ref-type="bibr" rid="bib1.bibx34" id="paren.26"/>.
A cloud-free, weak-wind day (20 June 2011) is considered in order to analyse
the evolution of the turbulence, from midday to sunset, by using both
observations and an LES model. Our analysis aims at (1) evaluating, with a
complete observation data set, the ability of the LES to simulate the
turbulence structure of the afternoon decay and (2) analysing the evolution
of integral scales, TKE and the shape of the spectra in both observations and
numerical simulation and as a function of height.</p>
      <p>The article is organized as follows: in the next section, we present the
experimental data set and describe the case study of 20 June 2011 through the
observations (Sect. <xref ref-type="sec" rid="Ch1.S2"/>). In Sect. <xref ref-type="sec" rid="Ch1.S3"/>, the LES is
presented and evaluated with the observations. Our spectral analysis method,
used in both observations and LES, is then described in
Sect. <xref ref-type="sec" rid="Ch1.S4"/>, before we present and discuss our results
(Sect. <xref ref-type="sec" rid="Ch1.S5"/>). Concluding remarks are made in
Sect. <xref ref-type="sec" rid="Ch1.S6"/>.</p>
</sec>
<sec id="Ch1.S2">
  <title>Experimental data set and case study</title>
      <p>The BLLAST experiment took place in the south of France, near the
Pyrénées mountain range, during the summer of 2011. A set of various
observational platforms (aircraft, remotely piloted aircraft systems,
balloons) and continuous measurements (towers, remote sensing) monitored the
PBL diurnal evolution, focusing on the AT, in various meteorological regimes.
The BLLAST experiment provides a unique data set to investigate the vertical
structure of the decaying PBL (see <xref ref-type="bibr" rid="bib1.bibx34" id="altparen.27"/>, for a detailed
description of BLLAST objectives and the experiment).</p>
      <p>The experimental data set used in this study, the case study chosen and its
simulation are now described. Note that the site longitude is around
0.21<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E; consequently, UTC, very similar to local solar time, is
used hereafter as the time reference.</p>
<sec id="Ch1.S2.SS1">
  <title>Experimental data set</title>
      <p>In order to monitor the evolution of the mean structure of the PBL during the
AT (and initialize the simulation), we used standard radiosoundings launched
every 6 h, from 06:00 to 18:00 UTC, and hourly radiosoundings
<xref ref-type="bibr" rid="bib1.bibx26" id="paren.28"/> of the lower troposphere (up to 3 to 4 km), from 13:00 to
18:00 UTC. The launching sites of the two types of radiosoundings were 4 km
apart. The radiosondes measured temperature, water vapour content and the
sonde location from which the horizontal wind components were deduced.</p>
      <p>Surface energy balance and turbulence structure in the surface layer were
provided by several ground stations over different vegetation coverages
(wheat, corn, grass, pine forest and moor (composed of heather and gorse)). A
permanent 60 m tower provided integrated turbulence measurements in the
surface layer above the heterogeneous surface. The statistical moments were
estimated over detrended 30 min periods from 10 Hz raw measurements. The
surface heat fluxes are used as surface forcing in the simulation.</p>
      <p>Two aircraft, the French Piper Aztec (PA) from SAFIRE (Service des Avions
Français Instruments pour la Recherche en Environnement) <xref ref-type="bibr" rid="bib1.bibx46" id="paren.29"/>
and the Italian Sky Arrow (SA) from Ibimet (Istituto di Biometeorologia del
CNR) and Isafom (Istituto per i Sistemi Agricoli e Forestali del
Mediterraneo) <xref ref-type="bibr" rid="bib1.bibx14" id="paren.30"/>, carried out flights throughout a wide
area during the afternoon, at 65 and
40 m s<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>, respectively. They measured temperature, moisture, pressure,
CO<inline-formula><mml:math display="inline"><mml:msub><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:math></inline-formula> mixing ratio and 3-D wind at 50 Hz (SA) and 25 Hz (PA) on 25 to
40 km legs stabilized in attitude and altitude. The detailed instrumentation
of both aircraft is given in <xref ref-type="bibr" rid="bib1.bibx34" id="text.31"/>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1"><caption><p>Normalized altitude <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>z</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> (where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is the PBL depth) of the
legs flown by the two aircraft on 20 June 2011 (Piper Aztec in blue, Sky
Arrow in red) and launching times of the radiosoundings (black arrows).</p></caption>
          <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f01.png"/>

        </fig>

</sec>
<sec id="Ch1.S2.SS2">
  <title>Case description</title>
      <p>On the basis of meteorological criteria and data coverage, 20 June 2011 was
selected as our case study. The synoptic situation was a high-pressure system
over the southwest of France, with a light westerly wind leading to fair and
cloud-free weather.</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F1"/> shows the normalized altitude <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>z</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> of the stacked legs
flown by the aircraft as well as the different launching times of the
radiosoundings (the method used for the PBL height (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) estimation is
discussed later). The two aircraft flew simultaneously, the PA flying above
the SA. They flew along west–east parallel legs, at three latitudes and, as
shown in Fig. <xref ref-type="fig" rid="Ch1.F1"/>, at six heights within the PBL and at two
different time periods: the first one from 14:30 to 15:30 UTC, the second
one later, from 17:45 to 19:00 UTC. This flight strategy provides access to
six heights to study the vertical structure of the turbulence within the PBL.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2"><caption><p>Observed vertical profiles of <bold>(a)</bold> the potential temperature
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula> and <bold>(b)</bold> the wind direction on 20 June 2011. The black
dashed lines represent the initial profiles of the LES.</p></caption>
          <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f02.png"/>

        </fig>

      <p>Figure <xref ref-type="fig" rid="Ch1.F2"/> presents the evolution of the potential temperature
(<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula>) and the wind direction in the PBL at several hours from 05:00 to
18:00 UTC on 20 June 2011. During the day, the PBL warms by about 7 K and
the PBL depth <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> grows up to about 1100 m above ground level.
Figure <xref ref-type="fig" rid="Ch1.F2"/>a also shows evidence of a warm advection above the PBL
between 05:15 and 11:00 UTC that must be taken into account in the simulation. After
11:00 UTC, the <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula> profile hardly changes in the free atmosphere,
meaning that the temperature advection is very weak.</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F2"/>b shows an easterly wind within the PBL, veering to
westerly above. The wind intensity remains constant all throughout the day
(not shown): it is weak within the PBL (less than 4 m s<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>) and
increases with height, up to 10 m s<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> at 1500 m.</p>
      <p>The water vapour mixing ratio (<inline-formula><mml:math display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula>) increases from 8 to 10 g kg<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> in
the PBL until 13:00 UTC and decreases afterward. The temporal evolution of
the PBL mean vertical structure is further analysed in
Sect. <xref ref-type="sec" rid="Ch1.S3.SS2"/>.</p>
      <p>The surface sensible and latent heat fluxes (<inline-formula><mml:math display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula> and LE, respectively)
measured above various vegetation coverages are presented in Fig. <xref ref-type="fig" rid="Ch1.F3"/>.
The maximum value of <inline-formula><mml:math display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula> varies from 100 to 130 W m<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> over grass and
moor to 450 W m<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> over pine forest. LE shows much less variability
between vegetation coverage, maximum values varying from 250 to
350 W m<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>. The measurements at 60 m height integrate a large
footprint and should give flux estimates of the heterogeneous landscape. As
such, <inline-formula><mml:math display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula> measured at 60 m height is encompassed in all the other
measurements and is close to the moor and
grass, the dominant vegetation , which represents about 40 % of the
vegetation cover on the plateau.</p>
      <p>In this study, the AT is defined as the period from the time when the surface
buoyancy flux is maximum, to the time where it goes to 0 (the surface
buoyancy flux is defined as the turbulent vertical transport of virtual
potential temperature and is approximated as a linear combination of observed
surface sensible and latent heat flux). This period varies according to the
surface <xref ref-type="bibr" rid="bib1.bibx34" id="paren.32"/>. For the moor coverage, whose surface fluxes will
be used to drive the simulation of 20 June 2011, this period starts at
12:00 UTC and ends at 1750 UTC, while it ends 20 min earlier when
considering <inline-formula><mml:math display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula> instead of the buoyancy flux. This delay is observed for all
the intense observation period (IOP) days of the BLLAST campaign implying
that the latent heat flux reaches its minimum value systematically later than
the sensible heat flux. Thus, the forcing timescale of the surface flux decay
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">f</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is around 5.8 h over the moor surface.</p>
</sec>
</sec>
<sec id="Ch1.S3">
  <title>LES</title>
      <p>As a complementary tool, a LES is initialized with the BLLAST observations to
study turbulence decay of convective boundary layer over a homogeneous and
flat surface. The observations from 20 June are used to guide our simulation,
like 1 July and 25 June guided the studies of <xref ref-type="bibr" rid="bib1.bibx2" id="text.33"/> and
<xref ref-type="bibr" rid="bib1.bibx42" id="text.34"/>, respectively. Our aim is not to reproduce a real case
but rather to use the BLLAST data set as a benchmark to simulate a boundary
layer with the same range of thermal and dynamical instabilities as those
observed during BLLAST.</p>
<sec id="Ch1.S3.SS1">
  <title>LES configuration and initialization</title>
      <p>Our LES is initialized with early morning radiosoundings and forced with
homogeneous surface fluxes, based on those measured over the moor surface.
Temperature and humidity advection are prescribed. The lateral boundary
conditions are periodic.</p>
      <p>The LES code from the National Center for Atmospheric Research
(<xref ref-type="bibr" rid="bib1.bibx36 bib1.bibx51 bib1.bibx41 bib1.bibx29" id="altparen.35"/>) is based on the
Boussinesq equations, including conservation laws for momentum and mass and
the first law of thermodynamics. The subgrid-scale model includes a
turbulent-kinetic-energy–eddy-viscosity model suggested by
<xref ref-type="bibr" rid="bib1.bibx10" id="text.36"/>, used by <xref ref-type="bibr" rid="bib1.bibx36" id="text.37"/> and improved by
<xref ref-type="bibr" rid="bib1.bibx50" id="text.38"/>.</p>
      <p>The simulation resolves a domain of 10.24 km <inline-formula><mml:math display="inline"><mml:mo>×</mml:mo></mml:math></inline-formula> 10.24 km horizontally
and 3.072 km vertically, with <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>x</mml:mi><mml:mo>=</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>y</mml:mi><mml:mo>=</mml:mo><mml:mn>40</mml:mn></mml:mrow></mml:math></inline-formula> m and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>z</mml:mi><mml:mo>=</mml:mo><mml:mn>12</mml:mn></mml:mrow></mml:math></inline-formula> m of horizontal and vertical resolution, respectively. This results from
a compromise between the computation time and three constraints: (1) the
domain size and resolution were chosen after a sensitivity study (not shown)
so that the LES spectra were able to represent the main characteristics of
the observed spectra, (2) the resolution was chosen so that the ratio of
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> to (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>x</mml:mi><mml:mo>×</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>y</mml:mi><mml:mo>×</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>z</mml:mi></mml:mrow></mml:math></inline-formula>)<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> was large enough
to ensure that the results were independent of the resolution
<xref ref-type="bibr" rid="bib1.bibx51" id="paren.39"/>, and (3) the ratio of <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>x</mml:mi></mml:mrow></mml:math></inline-formula> to <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:mi>z</mml:mi></mml:mrow></mml:math></inline-formula> was kept
rather small but with a high enough vertical resolution to correctly
represent the entrainment zone <xref ref-type="bibr" rid="bib1.bibx51" id="paren.40"/>. The time step evolves
during the simulation and is about 1.4 s for fully convective conditions.</p>
      <p>The simulation was initialized early in the morning, in order to ensure a
fully turbulent convective PBL by the afternoon. The wind,
potential-temperature and specific-humidity initial profiles for the LES were
deduced from the 05:15 UTC radiosounding (see dashed lines in
Fig. <xref ref-type="fig" rid="Ch1.F2"/> for temperature and wind speed). No geostrophic wind is
prescribed. This simple representation of the wind leads to a simulation with
very low wind speed, as is the case in the observations, but does not allow
us to simulate the shear in wind direction. A homogeneous and flat surface is
considered in the LES, with imposed surface fluxes which are those measured
at the moor site (Fig. <xref ref-type="fig" rid="Ch1.F3"/>).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3"><caption><p>Temporal evolution of <bold>(a)</bold> surface sensible (<inline-formula><mml:math display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula>) and
<bold>(b)</bold> latent (LE) heat fluxes over several vegetation coverages on 20
June 2011. Dashed black curves stand for the surface flux used as boundary
conditions for the LES. The vertical dashed lines stand for the times of
maximum surface buoyancy flux (at 12:00 UTC) and zero value (at
17:50 UTC).</p></caption>
          <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f03.png"/>

        </fig>

      <p>Vertical profiles of large-scale total advection (horizontal plus vertical
advection) of heat and moisture were hourly prescribed in the simulation and
linearly interpolated in between. They were derived from the AROME
(Application of Research to Operations at Mesoscale) <xref ref-type="bibr" rid="bib1.bibx47" id="paren.41"/> forecast model (horizontal resolution of
2.5 km), using the 16 grid points in a box surrounding the experimental
site. This model confirms predominant zonal advection, especially during the
morning.</p>
      <p>From 05:15 to 10:00 UTC, temperature advection is important and about
10 K day<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> from 500 m up to 1500 m (not shown). After 11:00 UTC, it
decreases and is negligible in the afternoon. This is consistent with what is
observed regarding the evolution of the potential temperature
(Fig. <xref ref-type="fig" rid="Ch1.F2"/>a). From sunrise to 14:00 UTC, the moisture advection is
about <inline-formula><mml:math display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>10 g kg<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> day<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> from the surface up to 500 m, and
about 10 g kg<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> day<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> above. After 14:00 UTC, the moisture
advection weakens (not shown).</p>
      <p>The data files used to run this case (initial profiles, surface flux and
advection profiles) are available on the website of the BLLAST database
(<uri>http://bllast.sedoo.fr/database</uri>).</p>
</sec>
<sec id="Ch1.S3.SS2">
  <title>Evaluation of the simulated boundary layer</title>
      <p>The bracket notation <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mi mathvariant="italic">ψ</mml:mi><mml:mo>〉</mml:mo></mml:mrow></mml:math></inline-formula> for any simulated variable <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ψ</mml:mi></mml:math></inline-formula>
is used to represent the 2-D horizontal average over the LES domain. The same
notation is used for the 1-D horizontal average of the airborne measurements
along the legs. For the surface data set, <inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mi mathvariant="italic">ψ</mml:mi><mml:mo mathvariant="normal">¯</mml:mo></mml:mover></mml:math></inline-formula> represents the time
average notation. For these three types of data sets, the turbulent
fluctuations <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="italic">ψ</mml:mi><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> are defined as deviations from the corresponding
mean. For a fairer comparison with the simulated variances, the observed
variances are estimated by integration of the spectra over the wave number
range resolved in the simulation. Finally, all the simulated mean vertical
profiles are averaged over 30 min and depicted, for simplicity, with the
bracket notation <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mi mathvariant="italic">ψ</mml:mi><mml:mo>〉</mml:mo></mml:mrow></mml:math></inline-formula>, which then indicates both horizontal
and temporal average.</p>
      <p>The evolution of the simulated <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula> vertical profiles is compared with
observations in Fig. <xref ref-type="fig" rid="Ch1.F4"/>a from 05:30 to 17:50 UTC. The
simulated <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula> is close to the observations in the mixed layer
(differences lower than 0.1 K) and in the free atmosphere, simulating the
change in <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula> profile between 05:15 and 11:15 UTC due to the prescribed
advection.</p>

      <?xmltex \floatpos{p}?><fig id="Ch1.F4"><caption><p>Vertical profiles of <bold>(a)</bold> <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula>, <bold>(b)</bold> <inline-formula><mml:math display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula>,
<bold>(c)</bold> wind speed (WS) and <bold>(d)</bold> wind direction (WD) observed
(solid lines and dotted lines for WD) and obtained by LES (dashed lines).</p></caption>
          <?xmltex \igopts{width=167.87126pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f04.png"/>

        </fig>

      <p>In the first 100 m, the differences in stability profile at 11:30 UTC might
be due to the different locations of the soundings and the moor site where
the surface flux is observed. The 17:30 UTC LES profile is already neutral,
whereas the observation at 17:50 UTC still has a superadiabatic region. The
differences are due to the fact that as soon as the surface buoyancy fluxes
turn negative, the LES potential temperature profile becomes stable in the
lower layers of the PBL. This
delay between the time when the buoyancy flux goes to 0 and the time when the
local gradient of virtual potential temperature changes sign has been
observed and analysed in <xref ref-type="bibr" rid="bib1.bibx1" id="text.42"/>. It can be of the order of
30 min to 1 h.</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F4"/>b presents the evolution of the water vapour mixing
ratio. The temporal evolution of <inline-formula><mml:math display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula> profiles shows a well-simulated daily
humidification. A departure of 1 g kg<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> from the value
actually observed can be seen at 13:05 and 17:50 UTC.</p>
      <p>The horizontal mean wind speed is well reproduced in the simulation during
the day: the wind remains weak and about 2 m s<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> in the PBL. <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>u</mml:mi><mml:mo>∗</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula>
evolves from 0.2 to 0.1 during the afternoon for both observed and simulated
data. The wind increases with altitude above the PBL and reaches
10 m s<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> at 2000 m. No wind forcing is prescribed in the simulation;
therefore, the observed wind direction change from west to east within the
mixed layer between 05:30 and 11:30 UTC is not simulated
(Fig. <xref ref-type="fig" rid="Ch1.F4"/>d). Whilst the wind speed shear is well simulated,
the wind direction shear is evidently underestimated. Consequently,
shear-driven processes <xref ref-type="bibr" rid="bib1.bibx43" id="paren.43"/> might not be as important in the
simulation as in the observations.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5"><caption><p>Vertical profiles of the buoyancy flux normalized by the surface
buoyancy flux at 12:00 UTC according to the normalized height <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>z</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.</p></caption>
          <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f05.png"/>

        </fig>

      <p>The simulated vertical profiles of the buoyancy flux normalized by the
surface buoyancy flux at the start of the AT (Fig. <xref ref-type="fig" rid="Ch1.F5"/>) have quite
a classical shape until 13:30 UTC, with a linear decrease with height and
negative flux above 0.8 <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. In the simulation, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is estimated as the
height of the mixed layer, determined with a threshold on the <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">θ</mml:mi></mml:math></inline-formula>
vertical gradient (0.01 K m<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula>). This method was preferred to the one
used for radiosoundings (see below) because of the complex humidity profiles
which lead to more fluctuating <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> estimates. However, the difference
between these two estimates is less than 50 m. After 13:30 UTC, the upper
layer, characterized by negative entrainment flux, deepens and goes down to
0.6 <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> at 18:00 UTC. During the AT the entrainment rate (ratio of the
buoyancy flux at the top of the PBL to the buoyancy flux at surface) remains
constant and about <inline-formula><mml:math display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.13 (not shown). Unfortunately, this value cannot be
compared to observations since the fluxes deduced from airborne measurements
in the PBL vary substantially at that time and because of the lack of
statistics on the large scales in a less and less stationary PBL. Flight legs
long enough to obtain accurate statistical moment estimates in convective PBL
<xref ref-type="bibr" rid="bib1.bibx28" id="paren.44"/> are even more relevant during the AT.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6"><caption><p>Temporal evolution of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> in the simulation (black), observed by
the UHF wind profiler (blue) and depicted using radiosondes (RS),
measurements (red dots).</p></caption>
          <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f06.png"/>

        </fig>

      <p>The temporal evolution of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> has been estimated from ultra high-frequency
radar wind profiler (hereafter UHF) and radiosounding measurements and has
been compared to the simulation (Fig. <xref ref-type="fig" rid="Ch1.F6"/>). <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is estimated from UHF
as the maximum of the refractive index structure coefficient
<xref ref-type="bibr" rid="bib1.bibx19 bib1.bibx21" id="paren.45"/>. From radiosoundings, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is estimated as the
altitude of the maximum relative humidity below 2500 m (this criterion has
been shown to be consistent in time and height during the BLLAST experiment;
<xref ref-type="bibr" rid="bib1.bibx34" id="altparen.46"/>).</p>
      <p>Until 09:00 UTC, the UHF detects the residual layer of the previous day.
After 10:00 UTC, the <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> increase is similarly depicted by the UHF and
radiosoundings, with a maximum value of 1100 m. The simulated PBL grows
slower than the observed PBL and reaches 850 m. This discrepancy between
observed and simulated <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> (which is larger than the uncertainty of the
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> estimate) might be partly explained by a weaker entrainment effect in
the simulation due to a lack of wind shear.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F7"><caption><p>Temporal evolution of the resolved TKE (subscript RES) at different
heights in the simulation (different colours). TKE deduced from aircraft and
surface (subscript OBS) spectra integrated over the LES spectra wave number
range (open and filled circles, respectively). The vertical dashed lines
stand for the times of maximum surface buoyancy flux (at 12:00 UTC) and its
zero value (at 17:50 UTC).</p></caption>
          <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f07.png"/>

        </fig>

      <p>The temporal evolution of the simulated and observed TKE at several heights
is presented in Fig. <xref ref-type="fig" rid="Ch1.F7"/>.
            <disp-formula id="Ch1.E1" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mtext>TKE</mml:mtext><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>,</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:mfrac></mml:mstyle><mml:mo>(</mml:mo><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi>u</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>,</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>+</mml:mo><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi>v</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>,</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>+</mml:mo><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi>w</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mo>(</mml:mo><mml:mi>z</mml:mi><mml:mo>,</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>)</mml:mo><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
          where <inline-formula><mml:math display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi>u</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi>v</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi>w</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:math></inline-formula> are the variances in the
horizontal <inline-formula><mml:math display="inline"><mml:mi>u</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mi>v</mml:mi></mml:math></inline-formula> and vertical <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> wind components. For a better
comparison, simulated and observed TKE are estimated using the wind component
variance deduced from the integration of the spectra over the wave number
range of the simulation. By doing this, the TKE associated with large and
small eddies observed, but not simulated or resolved in the LES, is removed
from the observed TKE. Even with this method, LES underestimates the observed
TKE by a factor which is sometimes as high as 1.5.</p>
      <p>In summary, the simulated boundary layer is comparable to the observed one in
terms of boundary layer height, wind speed, and dynamical and thermal
stability (not shown) near the surface. The lower development of the PBL
height of about 200 m and the TKE underestimated by a factor of 1.5 can be
partly explained by the directional wind shear which is not simulated. The
latter might increase the entrainment and the turbulence dynamical production
at the top of the boundary layer. Despite these differences regarding the
main PBL structure, the simulation is realistic enough to evaluate how the
turbulence evolves in a convective boundary layer during the AT and the
comparison of the simulated and observed boundary layer will be analysed
accordingly.</p>
</sec>
</sec>
<sec id="Ch1.S4">
  <title>Spectral analysis method</title>
      <p>A broad overview of the turbulent conditions during the afternoon is
depicted through the analysis of the TKE temporal evolution
at different heights in the PBL.</p>
      <p>The energy distribution among the different eddy scales is then studied
through a spectral analysis of the vertical velocity <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> within the entire
PBL. The evolution of <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> spectral characteristics is analysed by use of an
analytical spectral model.</p>
      <p>This study focuses on <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> because simulated and observed <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> spectra are more
easily comparable than the spectra of the horizontal components. Indeed, the
horizontal components have significant energy at low wave number (large
scales) in the observations, which cannot be represented in our simulated
domain.</p>
      <p>The choice of the analytical spectra is now discussed since several models
exist for convective conditions. Among others, the <xref ref-type="bibr" rid="bib1.bibx22 bib1.bibx23" id="text.47"/>
formulations were established from Kansas experiment observations for the
surface layer and from Minnesota experiment observations for the mixed layer.
The Kàrmàn spectral model <xref ref-type="bibr" rid="bib1.bibx24" id="paren.48"/> is also widely used for
isotropic turbulence. Højstrup (<xref ref-type="bibr" rid="bib1.bibx20" id="year.49"/>) proposed a more
generalized model for <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> spectra up to <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>z</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>=</mml:mo></mml:mrow></mml:math></inline-formula> 0.5, based on a stability
function from neutral to very unstable conditions. However, many of these
analytical models were validated for unstable near-surface conditions and
most of them are not suitable within the entire convective PBL
<xref ref-type="bibr" rid="bib1.bibx33" id="paren.50"/>. Among several analytical models tested, the general
kinematic spectral model for non-isotropic horizontally homogeneous turbulent
field from <xref ref-type="bibr" rid="bib1.bibx25" id="text.51"/> (hereafter referred to as KL89) is the one
which best fits the observed spectra at the surface and in the boundary layer
acquired during the BLLAST field campaign (not shown). For <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula>, the KL89
model gives
          <disp-formula id="Ch1.E2" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mtext>Kris</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi>w</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>=</mml:mo><mml:mtext>co</mml:mtext><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="italic">π</mml:mi></mml:mrow></mml:mfrac></mml:mstyle><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mn mathvariant="normal">1</mml:mn><mml:mo>+</mml:mo><mml:mfrac><mml:mn mathvariant="normal">8</mml:mn><mml:mn mathvariant="normal">3</mml:mn></mml:mfrac><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi>a</mml:mi><mml:mo>(</mml:mo><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac><mml:msup><mml:mo>)</mml:mo><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="italic">μ</mml:mi></mml:mrow></mml:msup></mml:mrow><mml:mrow><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:mfrac><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub><mml:mi>k</mml:mi></mml:mrow><mml:mrow><mml:mi>a</mml:mi><mml:mo>(</mml:mo><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac><mml:msup><mml:mo>)</mml:mo><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="italic">μ</mml:mi></mml:mrow></mml:msup><mml:msup><mml:mo>)</mml:mo><mml:mrow><mml:mn mathvariant="normal">5</mml:mn><mml:mo>/</mml:mo><mml:mo>(</mml:mo><mml:mn mathvariant="normal">6</mml:mn><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>)</mml:mo><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where
          <disp-formula id="Ch1.E3" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi>a</mml:mi><mml:mo>(</mml:mo><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mi mathvariant="italic">π</mml:mi><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mi mathvariant="italic">μ</mml:mi><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>(</mml:mo><mml:mfrac><mml:mn mathvariant="normal">5</mml:mn><mml:mrow><mml:mn mathvariant="normal">6</mml:mn><mml:mi mathvariant="italic">μ</mml:mi></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>(</mml:mo><mml:mfrac><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="italic">μ</mml:mi></mml:mrow></mml:mfrac><mml:mo>)</mml:mo><mml:mi mathvariant="normal">Γ</mml:mi><mml:mo>(</mml:mo><mml:mfrac><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mn mathvariant="normal">3</mml:mn><mml:mi mathvariant="italic">μ</mml:mi></mml:mrow></mml:mfrac><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        <inline-formula><mml:math display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula> being the wave number along the trajectory of the aeroplane or along the
west–east axis in the simulation (which is also the mean wind direction in
the simulation) and in the mean wind direction for surface measurements.
<inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Γ</mml:mi></mml:math></inline-formula> is the gamma function. co is a coefficient which adjusts the amount
of energy because <inline-formula><mml:math display="inline"><mml:mrow><mml:msubsup><mml:mi mathvariant="italic">σ</mml:mi><mml:mi>w</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:math></inline-formula> is calculated over a limited range of wave
numbers. This model has two other characteristic parameters: the integral
length scale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, which is a characteristic scale corresponding to the
scales over which <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> remains correlated with itself
<xref ref-type="bibr" rid="bib1.bibx27" id="paren.52"/>, and a sharpness parameter <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula>, which governs the
curvature of the spectra in the region of the peak, between the low wave
number range and the inertial subrange. The larger <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula>, the sharper the
peak. According to Eq. (<xref ref-type="disp-formula" rid="Ch1.E2"/>), the KL89 model gives the
<xref ref-type="bibr" rid="bib1.bibx22" id="text.53"/> spectrum for <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>.5 and the <xref ref-type="bibr" rid="bib1.bibx24" id="text.54"/> spectrum for
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>. It is thus a more generalized model, able to adapt to a larger range
of conditions. Note that <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is related to the wavelength of the energy
density maximum (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) by a monotonic function of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula>:
          <disp-formula id="Ch1.E4" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msup><mml:mfenced close="}" open="{"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">5</mml:mn><mml:mn mathvariant="normal">3</mml:mn></mml:mfrac></mml:mstyle><mml:msqrt><mml:mrow><mml:msup><mml:mi mathvariant="italic">μ</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">6</mml:mn><mml:mn mathvariant="normal">5</mml:mn></mml:mfrac></mml:mstyle><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msqrt><mml:mo>-</mml:mo><mml:mo>(</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">5</mml:mn><mml:mn mathvariant="normal">3</mml:mn></mml:mfrac></mml:mstyle><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>+</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>)</mml:mo></mml:mfenced><mml:mstyle scriptlevel="+1"><mml:mfrac><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="italic">μ</mml:mi></mml:mrow></mml:mfrac></mml:mstyle></mml:msup><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="italic">π</mml:mi></mml:mrow><mml:mrow><mml:mi>a</mml:mi><mml:mo>(</mml:mo><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula></p>
      <p>This model is fit to each observed and LES spectrum by finding the best [co,
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula>] triplet using a logarithmic least squares difference method.</p>
      <p>The integral scale of <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> is usually defined from the <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> autocorrelation
function <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>R</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> as
          <disp-formula id="Ch1.E5" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi>w</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∫</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mi mathvariant="normal">∞</mml:mi></mml:munderover><mml:msub><mml:mi>R</mml:mi><mml:mi>w</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:mi>r</mml:mi><mml:mo>)</mml:mo><mml:mi mathvariant="normal">d</mml:mi><mml:mi>r</mml:mi><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math display="inline"><mml:mi>r</mml:mi></mml:math></inline-formula> is the displacement in space or time. <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> gives an estimate of
the horizontal size of the convective thermals in the boundary layer. In this
study, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is obtained using an integration until the first 0 of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>R</mml:mi><mml:mi>w</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:mi>r</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>
<xref ref-type="bibr" rid="bib1.bibx27" id="paren.55"/>. It is used here as a reference to which <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is
compared.</p>
      <p>In this KL89 analytical spectrum, anisotropy of turbulence is taken into
account by varying the integral scale from transverse to lateral spectra.
Even considering anisotropy, the spectrum follows the usual <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">5</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> slope in
the inertial subrange.</p>
      <p>For surface-based spectra, 30 min samples are used, which is a good
compromise between a sufficient number of eddies and stationary conditions.
The spectra based on the aircraft measurements are calculated on legs that
are, on average, 35 km. To ensure consistency between simulated and observed
spectra, 1-D simulated spectra are considered in the LES. They are calculated
along the west–east direction and averaged along the north–south direction.
Simulated spectra are estimated above the fourth vertical level (to ensure a
negligible contribution of the subgrid scale) and every 96 m in the
vertical. The same sampling is used to calculate the autocorrelation
functions for <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> estimates.</p>
      <p>In order to study the evolution of the spectral slopes in specific domains,
the wave number range is split into three parts: (1) the low wave number
range <inline-formula><mml:math display="inline"><mml:mrow><mml:mo mathvariant="italic">{</mml:mo><mml:mn mathvariant="normal">0</mml:mn><mml:mo>,</mml:mo><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo mathvariant="italic">}</mml:mo></mml:mrow></mml:math></inline-formula>, (2) the region, <inline-formula><mml:math display="inline"><mml:mrow><mml:mo mathvariant="italic">{</mml:mo><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo mathvariant="italic">}</mml:mo></mml:mrow></mml:math></inline-formula>, around the maximum
energy density at <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>k</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mi mathvariant="italic">π</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, and (3) the inertial subrange <inline-formula><mml:math display="inline"><mml:mrow><mml:mo mathvariant="italic">{</mml:mo><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>,</mml:mo><mml:mi mathvariant="normal">∞</mml:mi><mml:mo mathvariant="italic">{</mml:mo></mml:mrow></mml:math></inline-formula>. The limits are defined here as <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="italic">π</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:mi mathvariant="italic">π</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.</p>
      <p>An important part of the study is to verify the level of agreement between
the observed or LES spectra and the KL89 analytical model fit. A quality
index of the analytical fit is, therefore, estimated based on the ratio
between the observed (and LES) spectrum and the analytical spectrum:
          <disp-formula id="Ch1.E6" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>OBS</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:msub><mml:mi>N</mml:mi><mml:mtext>OBS</mml:mtext></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:munder><mml:mo movablelimits="false">∑</mml:mo><mml:mi>k</mml:mi></mml:munder><mml:mfenced close="|" open="|"><mml:mi>log⁡</mml:mi><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mtext>OBS</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mtext>KL89</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced></mml:mfenced><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>

          <disp-formula id="Ch1.E7" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>LES</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mn mathvariant="normal">1</mml:mn><mml:mrow><mml:msub><mml:mi>N</mml:mi><mml:mtext>LES</mml:mtext></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:munder><mml:mo movablelimits="false">∑</mml:mo><mml:mi>k</mml:mi></mml:munder><mml:mfenced close="|" open="|"><mml:mi>log⁡</mml:mi><mml:mfenced open="(" close=")"><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mtext>LES</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mtext>KL89</mml:mtext></mml:msub><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:mfrac></mml:mstyle></mml:mfenced></mml:mfenced><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>
        where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mtext>OBS</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is the spectrum calculated from the observed <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula>,
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mtext>LES</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is the spectrum calculated from the simulated <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> and
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>S</mml:mi><mml:mtext>KL89</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is the analytical spectrum given by Eq. <xref ref-type="disp-formula" rid="Ch1.E2"/>
that best fits the observed or simulated spectra. <inline-formula><mml:math display="inline"><mml:mi>N</mml:mi></mml:math></inline-formula> is the number of <inline-formula><mml:math display="inline"><mml:mi>k</mml:mi></mml:math></inline-formula>
values on which <inline-formula><mml:math display="inline"><mml:mi>S</mml:mi></mml:math></inline-formula> is defined. The larger <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>OBS</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>LES</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>),
the larger the departure between the observed (simulated) and the analytical
spectra. No threshold can be found for these fit quality criteria; therefore,
values of <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>OBS</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>LES</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> in convective conditions (from
12:00 to 14:00 UTC) are used as a reference.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8"><caption><p>Normalized <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> spectra at <bold>(a)</bold> 15:00 and <bold>(b)</bold>
18:00 UTC from both aircraft (black) and LES (grey), fitted with the KL89
analytical spectral model (thick lines). The vertical continuous lines
represent <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, the maximum energy wave number, and the dashed
vertical lines represent <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>, the limits of the low wave number
range and of the inertial subrange, defined as <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="italic">π</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>k</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:mi mathvariant="italic">π</mml:mi><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.</p></caption>
        <?xmltex \igopts{width=193.47874pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f08.png"/>

      </fig>

      <p>Figure <xref ref-type="fig" rid="Ch1.F8"/> presents the normalized spectra of <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> from both
aircraft and simulated data, fitted with the KL89 analytical spectra model.
The aircraft (simulated) spectra are calculated at 15:00 and 18:00 UTC and
at <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>z</mml:mi><mml:mo>=</mml:mo><mml:mn>0.6</mml:mn><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi>z</mml:mi><mml:mo>=</mml:mo><mml:mn>0.6</mml:mn><mml:mo>-</mml:mo><mml:mn>0.75</mml:mn><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> slice-averaged). This figure shows first the
ability of the simulation to properly reproduce both the energy production
domain and the inertial subrange and, second, the ability of the analytical
spectral model to fit well the observed and simulated spectra in
mid-afternoon convective conditions (15:00 UTC) and at the end of the
afternoon (18:00 UTC).</p>
      <p>For these two examples, <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>OBS</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mn>0.11</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>LES</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mn>0.02</mml:mn></mml:mrow></mml:math></inline-formula> at
15:00 UTC and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>OBS</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mn>0.10</mml:mn></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>LES</mml:mtext></mml:msub><mml:mo>=</mml:mo><mml:mn>0.015</mml:mn></mml:mrow></mml:math></inline-formula> at 18:00 UTC.
In general, the quality index for the observations is about 5 to 10 times
larger than for the LES (not shown). This is due to the lack of statistics on
large scales in observations, leading to larger fluctuations in the spectral
density energy for the first domain (low wave numbers), whereas the LES
spectra are averaged along the north–south direction, reducing the
variability.</p>
      <p>We also found that the quality index for observed and simulated data
generally remained constant until 19:00 UTC, except for a slight increase in
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi>I</mml:mi><mml:msub><mml:mi>Q</mml:mi><mml:mtext>LES</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> for data above 0.6 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>z</mml:mi><mml:mo>/</mml:mo><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:mrow></mml:math></inline-formula> after 18:30 UTC. This means that
the spectra fit is equally reliable throughout the AT, allowing the study of
the time evolution of the spectra characteristics from the convective
conditions until near-neutral conditions. This result should be highlighted
in the case of simulated spectra, given the overly dissipative nature of the
subgrid-scale models in the LES <xref ref-type="bibr" rid="bib1.bibx35" id="paren.56"/>.</p>
      <p>The spectral changes throughout the AT are already noticeable in
Fig. <xref ref-type="fig" rid="Ch1.F8"/>: <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> shifts toward smaller wavelengths, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>
increases, the spectra flatten and the inertial subrange slope changes. This
is further quantified and discussed in the following section.</p>
</sec>
<sec id="Ch1.S5">
  <title>Results</title>
<sec id="Ch1.S5.SS1">
  <title>TKE decay within the entire PBL</title>
      <p>Most previous studies investigated either vertically integrated simulated TKE
over PBL depth or measured TKE in the surface layer. The TKE decay according
to height remains sparsely documented <xref ref-type="bibr" rid="bib1.bibx17 bib1.bibx16" id="paren.57"/>.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F9"><caption><p>Vertical profiles of the total (resolved and subgrid (subscript
TOT)) <bold>(a)</bold> TKE and <bold>(b)</bold> anisotropy at several different hours
during the AT in the LES.</p></caption>
          <?xmltex \igopts{width=199.169291pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f09.png"/>

        </fig>

      <p>Figure <xref ref-type="fig" rid="Ch1.F9"/>a shows the evolution of half-hour averaged hourly
vertical profiles of simulated TKE from 11:30 to 18:30 UTC. The profiles
show that TKE decreases within the whole depth of the PBL but that there is a
1-hour delay between the start of the decay at the top and the start at the
bottom: at 12:30 UTC, the TKE continues to increase in the lower PBL, while
it has started to decrease in the upper part. After 15:30 UTC, the decay is
homogeneous over the vertical. This differential TKE decay will be named TKE
top–down decay hereafter. This result is consistent with the
<xref ref-type="bibr" rid="bib1.bibx18" id="text.58"/> and <xref ref-type="bibr" rid="bib1.bibx34" id="text.59"/> studies which revealed, with
remote-sensing observations, a decay of TKE dissipation rates from top to
bottom. <xref ref-type="bibr" rid="bib1.bibx48" id="text.60"/> also studied the decay with direct numerical
simulation (DNS), based on a realistic surface flux decay. They found that
the turbulence is maintained at the surface relative to upper layers, which
they explain with shear at the surface.</p>
      <p>In this study, the simulation likely shows this top–down evolution because
the shear in wind direction at the top of the boundary layer is weak and does
not maintain the dynamical turbulence production. We can expect a reduced
top–down effect in reality since there is shear in direction which is not
simulated.</p>
      <p><?xmltex \hack{\newpage}?>Turbulence anisotropy (see Fig. <xref ref-type="fig" rid="Ch1.F9"/>b), considered here as the
ratio of the horizontal to the vertical wind variances, highlights the
turbulence structure evolution during the TKE decay. Before 16:30 UTC,
turbulence anisotropy remains smaller than unity in the mid-PBL, which is in
agreement with the dominant vertical motion of the convective eddies. In the
upper and lower parts of the PBL, turbulence anisotropy is larger than unity,
due to small vertical velocity variance close to the surface and the
entrainment zone (so-called “squashed” turbulence; <xref ref-type="bibr" rid="bib1.bibx31" id="altparen.61"/>).</p>
      <p>The anisotropy ratio becomes larger than 1 only after 17:30 UTC in the
middle of the PBL but increases close to the top as early as 12:30 UTC. The
change in anisotropy, like the TKE, starts early in the upper PBL, with an
increasing momentum transfer from vertical to horizontal components during
the decay process.</p><?xmltex \hack{\newpage}?>
</sec>
<sec id="Ch1.S5.SS2">
  <title>Spectral analysis</title>
<sec id="Ch1.S5.SS2.SSS1">
  <title>Evolution of the vertical velocity's spectral slopes</title>
      <p>The slopes of the simulated and observed spectra are first analysed because
(1) they are key characteristics of the turbulence spectra and (2) the KL89
spectral model assumes for <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>k</mml:mi><mml:mi>S</mml:mi><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> the theoretical slope of 1 and <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> for
a low and high wave number range, respectively. The slopes are estimated by
linear regression on <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>k</mml:mi><mml:mi>S</mml:mi><mml:mo>(</mml:mo><mml:mi>k</mml:mi><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> for the wave number first and third ranges
defined in Sect. <xref ref-type="sec" rid="Ch1.S4"/>.</p>
      <p>In the low wave number range, the slopes of the simulated and near-surface
observed spectra are close to the theoretical value of 1 and remain
approximately constant during the whole day (see Fig. <xref ref-type="fig" rid="Ch1.F10"/>a). The
spectral slopes of airborne measurements are steeper than the theory predicts
and vary from 1.5 to 2.5. This result illustrates the weak statistical
representativeness of large scales along aircraft flight paths, leading to
scattered spectra slope estimates in this wave number range.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F10"><caption><p>Temporal evolution of the slopes in <bold>(a)</bold> the low wave number
range and <bold>(b)</bold> the inertial subrange of the <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> spectra obtained by
LES (continuous lines), aircraft and surface measurements (open and filled
circles) at different heights (colours). The horizontal black lines stand for
the theoretical expected values.</p></caption>
            <?xmltex \igopts{width=213.395669pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f10.png"/>

          </fig>

      <p>In the inertial subrange, both simulated and aircraft data reveal steeper
slopes than the theoretical value of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula>, even during the fully
convective period (Fig. <xref ref-type="fig" rid="Ch1.F10"/>b). Steeper inertial subrange slopes were
previously observed with vertically pointing ground-based lidar
<xref ref-type="bibr" rid="bib1.bibx33" id="paren.62"/> and with airborne high-frequency in situ measurements;
<xref ref-type="bibr" rid="bib1.bibx32" id="paren.63"/>). The theoretical <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> slope is based on the hypothesis
of isotropic turbulence. Therefore, a possible explanation for these steeper
slopes in convective conditions could be the loss of isotropy in real
conditions and in particular the role of convective structures and the
associated anisotropy. As mentioned before, in Sect. <xref ref-type="sec" rid="Ch1.S5.SS1"/>,
convective structures are responsible for
anisotropy smaller than 1. We believe that the more “coherent” or organized
the <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> field, the smaller the anisotropy and the steeper the slope. But this
explanation needs further work for confirmation. At the end of the afternoon,
the slopes consistently flatten in both LES and aircraft data. This
flattening appears to behave differently according to height in two ways:
(1) it occurs earlier at the top of the PBL (around 16:00 UTC) than in the
lower layers (after 17:45 UTC at 0.15<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>); (2) the lower in the PBL the
flattening occurs, the smaller it is. These delayed and reduced changes with
decreasing altitude are consistent with the constant <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> slope during the
whole day near the surface.</p>
</sec>
<sec id="Ch1.S5.SS2.SSS2">
  <title>Characteristic length scales</title>
      <p>The integral scale is one of the two spectral characteristics determined from
the fit of the KL89 analytical spectral model.</p>
      <p>We verified that these integral scale estimates (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) were similar to
estimates of integral scales (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) based on the autocorrelation function
(Eq. <xref ref-type="disp-formula" rid="Ch1.E5"/>), which is more generally used. The two methods were found to
be consistent with each other and to give a similar temporal evolution of
integral scale (not shown). Hereafter, only <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is considered.</p>
      <p>The temporal evolution of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> obtained with aircraft and surface data and
with the simulation at different heights is presented in
Fig. <xref ref-type="fig" rid="Ch1.F11"/>. At midday, the length scales verify what is found
in literature, with a value of around 200 m (about 0.2<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) in the middle
of the mixed layer (<xref ref-type="bibr" rid="bib1.bibx27" id="altparen.64"/>, with aircraft observations
and <xref ref-type="bibr" rid="bib1.bibx11" id="text.65"/> with LES, among others). Smaller length scales are
observed and simulated at the top and at the bottom of the mixed layer
because of “squashed” eddies near the interfaces. <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> remains
approximately constant until 17:00 UTC and then increases above 0.15<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>
for both LES and aircraft data. The higher the considered level, the sharper
the <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> increase.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F11"><caption><p>Temporal evolution of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> calculated from the KL89 analytical
model fit on LES (continuous lines), aircraft (open circles) and surface
(closed circles) spectra at different heights (different colours). Note that
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> at surface and at 60 m is multiplied by a factor of 10. The vertical
dashed lines stand for the times of maximum surface buoyancy flux (at
12:00 UTC) and its zero value (at 17:50 UTC).</p></caption>
            <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f11.png"/>

          </fig>

      <p>Close to the surface, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> remains constant until 17:00 UTC at a height of
10 m and then decreases to 5 m. As expected, the 60 m mast data provide
longer <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> than those at the surface but with a large scatter (between 30
and 80 m), making it difficult to estimate <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> tendency with time at that
height.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F12"><caption><p>Temporal evolution of the parameter <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula>, obtained from the KL89
analytical model, by using LES (continuous lines), aircraft (open circles)
and surface (closed circles) data. The vertical dashed lines stand for the
times of maximum surface buoyancy flux (at 12:00 UTC) and its zero value (at
17:50 UTC).</p></caption>
            <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f12.png"/>

          </fig>

<?xmltex \hack{\newpage}?>
</sec>
<sec id="Ch1.S5.SS2.SSS3">
  <title>Shape of the spectra</title>
      <p>The spectral shape is depicted by the <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula> sharpness parameter
(Eq. <xref ref-type="disp-formula" rid="Ch1.E2"/>). Figure <xref ref-type="fig" rid="Ch1.F12"/> shows the temporal evolution of
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula> that gives the best fit of the spectra for simulation, aircraft and
surface data. Above 0.15 <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula> remains constant at a value of about 2
until 16:00 UTC, aircraft and simulated data giving similar results. These
results are similar to those found by <xref ref-type="bibr" rid="bib1.bibx33" id="text.66"/> with ground-based
lidar, who also observed sharper spectra than the Kaimal spectra (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>=</mml:mo><mml:mn>0.5</mml:mn></mml:mrow></mml:math></inline-formula>)
in the middle of the PBL. After 16:00 UTC, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula> decreases, meaning that the
turbulence spectra flatten during the late afternoon transition associated
with a broadening of the energy containing wave number range above 0.15<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.
This seems consistent with the theoretical spectral analysis by
<xref ref-type="bibr" rid="bib1.bibx16" id="text.67"/> (see their Fig. 6, bottom, in the convective boundary
layer). By contrast, close to the surface and at 60 m height, <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">μ</mml:mi><mml:mo>≈</mml:mo><mml:mn>0.5</mml:mn></mml:mrow></mml:math></inline-formula> throughout the day, which corresponds to the spectral model from
<xref ref-type="bibr" rid="bib1.bibx22" id="text.68"/> and means that the energy wave number range remains large
during the afternoon. In the KL89 analytical model,
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are linked by Eq. (<xref ref-type="disp-formula" rid="Ch1.E4"/>), which gives
higher <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> for higher <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula> <xref ref-type="bibr" rid="bib1.bibx27" id="paren.69"/>. As shown
in Fig. <xref ref-type="fig" rid="Ch1.F8"/>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> drifts slightly toward smaller
eddies. Keeping in mind that <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Λ</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> represents the distance between two
structures and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> represents the width of a structure, this means that
during the afternoon, the thermals become closer to each other, whereas the
increase in <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> means the thermals become larger. This is consistent with a
decreasing skewness of <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> as time evolves, which we find in both observation
and LES (not shown).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F13"><caption><p>Vertical profiles of the timings of changes observed in the
evolution of the TKE, the vertical and horizontal variances, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>v</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula>,
and the inertial subrange slope of <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> spectra. <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>t</mml:mi><mml:mo>′</mml:mo></mml:msup></mml:mrow></mml:math></inline-formula> is defined as the time
when <inline-formula><mml:math display="inline"><mml:mi>H</mml:mi></mml:math></inline-formula> is maximum (i.e. at 12:00 UTC).</p></caption>
            <?xmltex \igopts{width=227.622047pt}?><graphic xlink:href="https://acp.copernicus.org/articles/15/10071/2015/acp-15-10071-2015-f13.png"/>

          </fig>

<?xmltex \hack{\newpage}?>
</sec>
</sec>
<sec id="Ch1.S5.SS3">
  <title>Timing of the changes</title>
      <p>The previous results illustrate the changes in turbulence characteristics
throughout the afternoon according to height. The times when these
characteristics start to change are now quantified using the simulation data
above 0.15<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, the tower measurements at 60 m, and the near surface moor
and corn data. The time of change for a parameter <inline-formula><mml:math display="inline"><mml:mi>x</mml:mi></mml:math></inline-formula> is denoted by <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mi>x</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>
(Fig. <xref ref-type="fig" rid="Ch1.F13"/>). For <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and the slope, it is the time when the
decay rates of these spectra parameters depart from their mean value by more
than 3 times their standard deviation (the decay rates are estimated over
1.5 h and their means and standard deviations are calculated between noon
and 14:00 UTC). Because of the diurnal cycle of the TKE and the horizontal
and vertical velocity variances, this method could not be applied to
determine the time change in these parameters. <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mtext>TKE</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mo>&lt;</mml:mo><mml:msup><mml:msup><mml:mi>w</mml:mi><mml:mo>′</mml:mo></mml:msup><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>&gt;</mml:mo></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>
and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mo>&lt;</mml:mo><mml:msup><mml:msup><mml:mi>u</mml:mi><mml:mo>′</mml:mo></mml:msup><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>&gt;</mml:mo><mml:mo>+</mml:mo><mml:mo>&lt;</mml:mo><mml:msup><mml:msup><mml:mi>v</mml:mi><mml:mo>′</mml:mo></mml:msup><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>&gt;</mml:mo></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> were thus the times when the decaying rate of the
parameter (estimated by linear regression over 1.5 h) becomes larger than for an
arbitrary threshold of <inline-formula><mml:math display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>1.11 <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> m<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> s<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> (meaning a TKE decrease of <inline-formula><mml:math display="inline"><mml:mo>-</mml:mo></mml:math></inline-formula>0.02 m<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:math></inline-formula> s<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:math></inline-formula> for a time interval of 30 min).</p>
      <p>As already noticed in Sect. <xref ref-type="sec" rid="Ch1.S5.SS1"/>, the TKE first decreases at the top
of the boundary layer half an hour after the start of the AT
(Fig. <xref ref-type="fig" rid="Ch1.F13"/>). That is, once the surface flux starts to decrease, the
surface-driven turbulence does not rise up to the top of the boundary layer anymore.
This indicates that turbulence decreases first at the top of the PBL, whereas
it is maintained longer under 0.15 <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. The TKE decrease is exclusively
driven by the vertical velocity variance, which decreases at the top of the
PBL 1.5 h before the maximum of the surface buoyancy flux. The early
decrease in the vertical velocity variance is counterbalanced in TKE by the
delayed change in the horizontal wind variance. This implies an increase in
the anisotropy of the velocity variances in the early stage of surface flux
decrease.</p>
      <p>The change in other spectral parameters (length scale, sharpness and slope)
is observed much later, during the last 2 h before the zero surface buoyancy
flux. The vertical profiles of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mtext>slope</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="italic">μ</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>
indicate an increase in integral scales, a flattening of the inertial
subrange slope and a flattening of the spectra, appearing first at the top of
the boundary layer and rapidly reaching the lower layers.</p>
      <p>Near the surface and at 60 m, a very weak evolution of the spectra is
observed. The spectra keep the same sharpness, similar to Kaimal spectra,
with a constant slope of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula> in the inertial subrange, and a very
slightly decreasing <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. These results are consistent with the spectral
behaviour above 0.15 <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. Indeed, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">μ</mml:mi></mml:math></inline-formula> decreases from around 2 in
convective conditions to 0.5 at the end of the AT in the whole upper layer,
and the <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mi>w</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> increase in the upper layers is less and less pronounced with
decreasing height.</p><?xmltex \hack{\newpage}?>
</sec>
<sec id="Ch1.S5.SS4">
  <title>Discussion</title>
      <p>The above analysis of the evolution of the turbulence structure during the AT
suggests that we should separate this period into two stages: early and late
afternoon.</p>
      <p>In the early afternoon, from the occurrence of the buoyancy maximum until
about 2 h before sunset, (1) the TKE decreases within the whole PBL, with a
1-hour delay between the upper part (earlier decay) and the lower part of the
PBL (postponed decay), (2) the vertical profile of anisotropy does not change
much within the PBL, except close to the top, and (3) the spectra maintain
the characteristics of the fully developed convective boundary layer, with
similar integral scales and sharpness parameters.</p>
      <p>In the late afternoon, from 2 h before sunset until when the surface
buoyancy flux reduces to 0, (1) the TKE decreases more rapidly than during
the early AT within the whole PBL, (2) turbulence anisotropy increases
abruptly within the PBL, starting initially near the PBL top, and (3) the
shape of the spectra evolves, with a decrease in the sharpness parameter, a
flattening of the inertial subrange slope, and an increase in the integral
length scales in the mid and upper PBL. The higher in the PBL the integral
scales are, the stronger their increase, with very slight changes in the
spectra shape observed close to the surface.</p>
      <p>The two stages of the TKE decay found in this study remain consistent with
previous results found by <xref ref-type="bibr" rid="bib1.bibx39" id="text.70"/> and <xref ref-type="bibr" rid="bib1.bibx44" id="text.71"/>. Both
authors showed a decrease in the TKE following a <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>t</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mi>n</mml:mi></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> power law with a
continuous increase in <inline-formula><mml:math display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula>. <xref ref-type="bibr" rid="bib1.bibx39" id="text.72"/> defined two main stages
characterized by <inline-formula><mml:math display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula> around 2 and 6. <xref ref-type="bibr" rid="bib1.bibx44" id="text.73"/> added a preliminary
stage with <inline-formula><mml:math display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula> equal to 1. Our first stage includes <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>t</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>t</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>
power laws, and the second one includes <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>t</mml:mi><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula>. However, it seems somehow
arbitrary to characterize our two stages by a specific value of <inline-formula><mml:math display="inline"><mml:mi>n</mml:mi></mml:math></inline-formula> since it
evolves continuously. This study focuses on the link between the structure of
the turbulence and the TKE evolution. Also, the TKE budget evolution in time
was not of any help to explain the two stages of the TKE decrease. Whilst the
different terms do decrease with time, their respective contribution to the
TKE tendency hardly changes from the first to the second stages (not shown).</p>
      <p>Our understanding of the two different stages of the AT is that during the
early afternoon, the buoyancy flux remains large and its decay is slow enough
to give the PBL time to adjust to the change and to remain in quasi-steady
balance. In other words, the convective timescale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula> is small enough
(<inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 9 min) relative to <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">f</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula> 5.8 h) to allow this
quasi-steady state. The spectral characteristics remain similar to what they
are at maximum surface buoyancy flux. Buoyancy remains a dominant influence
during this stage, leading to the vertical velocity variance and convective
structures being predominant. The latter, with a characteristic horizontal length typically
linked to the PBL depth, could maintain a sharp spectral peak. The
predominance of convective structures might also be the cause of the steep
inertial subrange slope. Close to the surface, where these convective
structures are not yet well shaped, the inertial subrange slope is <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:math></inline-formula>.</p>
      <p>On the contrary, during the late afternoon, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula> increases (about 20 min at
17:00 UTC) and the buoyancy flux gets too small for the PBL to maintain the
vertical consistency of the turbulence structure from the surface up to the
top of the PBL. The impact of surface buoyancy decreases faster than that of
entrainment during this period: although the entrainment flux magnitude
diminishes, entrainment occurs over a broader vertical depth extending down
to 0.6<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> (Fig. <xref ref-type="fig" rid="Ch1.F5"/>).</p>
      <p>An increase in the entrainment role could explain the increase in the
vertical velocity integral scales (<xref ref-type="bibr" rid="bib1.bibx30 bib1.bibx4" id="altparen.74"/>), which is
observed in the upper PBL during the late afternoon during our BLLAST case.
The increase in vertical velocity integral scales is consistent with the
results of <xref ref-type="bibr" rid="bib1.bibx49" id="text.75"/> but disagrees with those of <xref ref-type="bibr" rid="bib1.bibx43" id="text.76"/>.
This could be due to the progressive cessation of the surface flux in
<xref ref-type="bibr" rid="bib1.bibx49" id="text.77"/> and <xref ref-type="bibr" rid="bib1.bibx17" id="text.78"/> versus the sudden shut-off in
<xref ref-type="bibr" rid="bib1.bibx43" id="text.79"/>. In the surface layer, the decrease in the integral scales
is consistent with the observations made by <xref ref-type="bibr" rid="bib1.bibx17" id="text.80"/> and with the
results of <xref ref-type="bibr" rid="bib1.bibx22" id="text.81"/>.</p>
      <p>The flattening observed in the inertial subrange during the late afternoon is
difficult to explain because one might expect a steeper slope in inertial
subrange when the flow becomes less turbulent, assuming that the smaller
scales will dissipate faster than the larger scales. However, hypotheses
could be made to explain the observed flattening of the spectra in the
inertial subrange: (1) the increase in anisotropy might be associated with
such a change in the cascade; (2) if the turbulence is now freely decaying,
without influence of coherent structures and vertical velocity dominance, the
cascade could become more efficient, resulting in a flattening slope
according to <xref ref-type="bibr" rid="bib1.bibx37" id="text.82"/>. In any case, it seems that with the
turbulence being no longer fully forced, the criteria for locally isotropic
turbulence are no longer met. The theoretical model of the TKE spectrum
proposed by <xref ref-type="bibr" rid="bib1.bibx16" id="text.83"/> could be an interesting tool to further
understand this slope change since it considers anisotropy of turbulence
through the KL89 analytical spectrum and also considers the terms of the
TKE budget which might impact on the inertial subrange slope.</p>
      <p>The progressive shut-off of the surface heat fluxes is shown to be an
important aspect of the AT. <xref ref-type="bibr" rid="bib1.bibx40" id="text.84"/> and <xref ref-type="bibr" rid="bib1.bibx43" id="text.85"/>, who analysed
simulations with a sudden shut-off of the buoyancy flux, pointed out what
they called a demixing process, which implies a negative buoyancy flux within
the whole PBL. The impact of entrainment in this case might be overestimated.
Similar to <xref ref-type="bibr" rid="bib1.bibx49" id="text.86"/>, when progressively transitioning through the
afternoon from a surface-buoyancy-dominated to an entrainment-dominated
regime, the demixing process is strongly reduced and limited to the upper
half of the PBL.</p>
      <p>One might wonder whether these results could be impacted by the initial
conditions. The use of all the airborne measurements acquired during the
BLLAST experiment shows the general trend of an increasing integral scale
during the late afternoon (not shown). However, it would be useful to
complete this study with some additional simulations either targeting other
BLLAST IOPs or performing some sensitivity analyses. Wind shear could be an
important focus as <xref ref-type="bibr" rid="bib1.bibx40" id="text.87"/>, <xref ref-type="bibr" rid="bib1.bibx43" id="text.88"/> and <xref ref-type="bibr" rid="bib1.bibx16" id="text.89"/>
found that strong wind shear at the top and bottom of the PBL delays the
decay.</p>
</sec>
</sec>
<sec id="Ch1.S6" sec-type="conclusions">
  <title>Conclusions</title>
      <p>This study is based on the use of analytical spectra to depict and quantify
changes in the vertical velocity spectra throughout the AT and according to
height. BLLAST aircraft and surface station measurements are used to study
the turbulence spectral evolution on 20 June 2011. A large-eddy simulation
constrained by observed conditions during BLLAST, but significantly
simplified, allows us to investigate a continuous spectral analysis in time
and height.</p>
      <p>The simulated data, even with simplified forcings and initial conditions, are
in satisfactory agreement with the airborne, radiosonde and surface
observations. The model reasonably simulates the turbulence structure through
the afternoon with a resolution and a domain size allowing a good fit of the
simulated spectra with the <xref ref-type="bibr" rid="bib1.bibx25" id="text.90"/> analytical model above
0.15<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.</p>
      <p>Two main conclusions can be drawn from this study, giving essential
information on the turbulence evolution in time and height:
<list list-type="order"><list-item><p>This study shows for the first time the different steps occurring during
the AT, which is defined as the period starting at the maximum surface
buoyancy flux and ending when the buoyancy flux reaches 0. The early
afternoon (first phase from 0 to 0.75<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">f</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>) is characterized by a
low-rate decrease in the energy level, but the turbulence characteristics
remain similar to those during fully convective conditions: similar
turbulence length scales and cascade characteristics from large to small
eddies. During the late afternoon (second phase from 0.75 to
1<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">τ</mml:mi><mml:mi mathvariant="normal">f</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>), TKE decay rates increase and turbulence characteristics
evolve rapidly, implying a very different eddy size and energy transfer.</p></list-item><list-item><p>The second important point concerns the turbulence evolution along the
vertical. The changes observed either in TKE decay (during the early
afternoon) or in <inline-formula><mml:math display="inline"><mml:mi>w</mml:mi></mml:math></inline-formula> spectral shape (during the late afternoon) start at the
top of the boundary layer. Furthermore, the higher the spectra within the
PBL, the stronger their shape changes. These results show that the top of the
boundary layer is affected by the changes first.</p></list-item></list></p>
</sec>

      
      </body>
    <back><ack><title>Acknowledgements</title><p>The BLLAST field experiment was made possible thanks to the contribution of
several institutions and organisations: INSU-CNRS (Institut National des
Sciences de l'Univers, Centre national de la Recherche Scientifique,
LEFE-IMAGO program), Météo-France, Observatoire Midi-Pyrénées
(University of Toulouse), EUFAR (EUropean Facility for Airborne Research)
BLLATE-1&amp;2, COST ES0802 (European Cooperation in the field of Scientific and
Technical) and the Spanish MINECO projects CGL2009–08609,
CGL2012–37416-C04–03 and CGL2011-13477-E. The field experiment would not
have taken place without the significant contribution of all participating
European and American research groups. The Piper Aztec research airplane is
operated by SAFIRE, which is a unit supported by INSU-CNRS, Météo-France
and the French Spatial Agency (CNES). The BLLAST field experiment was hosted
by the instrumented site of Centre de Recherches Atmosphériques,
Lannemezan, France (Observatoire Midi-Pyrénées, Laboratoire
d'Aérologie). Its 60 m tower is partly supported by the POCTEFA/FLUXPYR
European program. BLLAST data are managed by SEDOO, from Observatoire
Midi-Pyrénées. Since 2013, the French ANR has supported BLLAST analysis.
See <uri>http://bllast.sedoo.fr</uri> for all contributions. We particularly thank
Eric Pardyjak, Oscar Hartogensis, Dominique Legain and Frédérique Saï
for providing the surface measurements used in this study. We are also
grateful to Bruno Piguet for the first processing of the Piper Aztec data set
and to Dominique Legain and the CNRM-4M team for the frequent radiosoundings.
Computer facilities for the large-eddy simulation were provided by CALMIP
(Calcul en Midi-Pyrénées, France).<?xmltex \hack{\newline}?><?xmltex \hack{\newline}?>Edited
by: E. Pardyjak</p></ack><ref-list>
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