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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-15-2159-2015</article-id><title-group><article-title>Comparing turbulent parameters obtained from LITOS <?xmltex \hack{\newline}?>and radiosonde measurements</article-title>
      </title-group><?xmltex \runningtitle{Turbulence soundings by LITOS and radiosondes}?><?xmltex \runningauthor{A.~Schneider et~al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1">
          <name><surname>Schneider</surname><given-names>A.</given-names></name>
          <email>schneider@iap-kborn.de</email>
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Gerding</surname><given-names>M.</given-names></name>
          
        <ext-link>https://orcid.org/0000-0002-5382-4017</ext-link></contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Lübken</surname><given-names>F.-J.</given-names></name>
          
        </contrib>
        <aff id="aff1"><institution>Leibniz Institute of Atmospheric Physics at the University of Rostock, Kühlungsborn, Germany</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">A. Schneider (schneider@iap-kborn.de)</corresp></author-notes><pub-date><day>27</day><month>February</month><year>2015</year></pub-date>
      
      <volume>15</volume>
      <issue>4</issue>
      <fpage>2159</fpage><lpage>2166</lpage>
      <history>
        <date date-type="received"><day>28</day><month>May</month><year>2014</year></date>
           <date date-type="rev-request"><day>22</day><month>July</month><year>2014</year></date>
           <date date-type="rev-recd"><day>24</day><month>December</month><year>2014</year></date>
           <date date-type="accepted"><day>26</day><month>January</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://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015.html">This article is available from https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015.html</self-uri>
<self-uri xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015.pdf">The full text article is available as a PDF file from https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015.pdf</self-uri>


      <abstract>
    <p>Stratospheric turbulence is important for the mixing of trace species and the
energy balance, but direct measurements are sparse due to the required
resolution and accuracy.  Recently, turbulence parameters such as the energy
dissipation rate <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> were inferred from standard radiosonde data by
means of a Thorpe analysis. To this end, layers with vertically decreasing
potential temperature are analysed, which is expected to indicate turbulence.
Such an application assumes a proportionality between the Thorpe length
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and the Ozmidov scale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. While this relation is
accepted for the ocean, experimental evidence for such proportionality in the
stratosphere is sparse.  We have developed a high-resolution (8 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">kHz</mml:mi></mml:math></inline-formula>)
turbulence measurement system called LITOS (Leibniz Institute Turbulence
Observations in the Stratosphere), which for the first time resolves the inner
scale of turbulence in the stratosphere. Therewith the energy dissipation rate
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> can be determined by spectral analysis. This independent value for
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> enables us to check the relation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>∝</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.
In our measurements no such proportionality can be seen, although the mean of
the ratio <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is close to what is assumed in radiosonde
analyses. Dissipation rates for individual layers obtained from radiosondes
deviate up to a factor of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>3000</mml:mn></mml:mrow></mml:math></inline-formula> from those obtained by spectral analysis.
Some turbulent layers measured by LITOS are not observed by the radiosonde at all,
and vice versa.
However, statements about the statistical mean seem to be possible by Thorpe analysis.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <title>Introduction</title>
      <p>Although the stratosphere is mostly stably stratified, breaking of gravity waves
and instabilities cause turbulence and energy dissipation. This modifies the
energy transport from the troposphere to the mesosphere. The amount of energy
converted into heat is described by the turbulent energy dissipation rate
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula>. Moreover, turbulence is an important parameter for the vertical
mixing of trace species. As in the stratosphere turbulent dissipation occurs on
small scales of centimetres and below, measurements are technically challenging
and therefore sparse <xref ref-type="bibr" rid="bib1.bibx1 bib1.bibx13" id="paren.1"><named-content content-type="pre">e.g.</named-content></xref>.</p>
      <p>In order to enlarge the knowledge of turbulence by exploiting existing
measurements available for large geographical areas and several years, the
extraction of turbulence parameters such as <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> from standard
radiosonde data (vertical resolution 5 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>) has been proposed
<xref ref-type="bibr" rid="bib1.bibx2" id="paren.2"/>. The evaluation uses the method developed by
<xref ref-type="bibr" rid="bib1.bibx14 bib1.bibx15" id="normal.3"/> to detect static instabilities as a proxy for
turbulence. Note that such a measurement is somewhat different from measuring
the turbulent motions directly, as done by LITOS. For example, within an
instability turbulence may have not yet been developed or, on the other hand,
turbulence might be still active while the instability has already deceased.
Additionally, turbulence may not be related to static instabilities at all.</p>
      <p>The Thorpe analysis of unstable layers is done by comparing a measured potential
temperature profile to an equivalent (statically) stable one obtained by
sorting. This means that the order of the data points is changed upwards and
downwards to yield a statically stable profile with monotonously increasing
potential temperature.  Precisely, the Thorpe displacement <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>D</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is
defined by the vertical displacements needed for the sorting; i.e. if an air
parcel at altitude <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is sorted to <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>k</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, then the Thorpe displacement at
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>D</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>z</mml:mi><mml:mi>k</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.  The Thorpe length is the root mean
square of the Thorpe displacements taken over an unstable layer:

              <disp-formula id="Ch1.E1" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mtext>rms</mml:mtext><mml:mo>(</mml:mo><mml:msub><mml:mi>D</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:mo>)</mml:mo><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>

        It describes the distance over which heavier air parcels are carried above lighter
ones. <xref ref-type="bibr" rid="bib1.bibx19 bib1.bibx18" id="normal.4"/> use the Thorpe method for statistical
analysis without computing dissipation rates.</p>
      <p>The Ozmidov length scale

              <disp-formula id="Ch1.E2" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mi mathvariant="italic">α</mml:mi><mml:msqrt><mml:mfrac><mml:mi mathvariant="italic">ε</mml:mi><mml:mrow><mml:msup><mml:mi>N</mml:mi><mml:mn mathvariant="normal">3</mml:mn></mml:msup></mml:mrow></mml:mfrac></mml:msqrt><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>

        where <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> is the (kinetic) energy dissipation rate, <inline-formula><mml:math display="inline"><mml:mi>N</mml:mi></mml:math></inline-formula> the
Brunt–Väisälä frequency and <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">α</mml:mi></mml:math></inline-formula> a numerical constant near
unity, represents the vertical scales of the largest turbulent eddies
<xref ref-type="bibr" rid="bib1.bibx11" id="paren.5"/>.  For the determination of the dissipation rate from
a Thorpe analysis, the key assumption is a proportionality between Thorpe and
Ozmidov lengths, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>∝</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.  This relation has been
extensively studied in the ocean, and the assumption is fulfilled to a good
extent <xref ref-type="bibr" rid="bib1.bibx15 bib1.bibx3 bib1.bibx16" id="paren.6"/>.  But for the
atmosphere there are only few examinations of the proportionality
<xref ref-type="bibr" rid="bib1.bibx4 bib1.bibx7 bib1.bibx21" id="paren.7"><named-content content-type="pre">e. g.</named-content></xref>.  With our new
high-resolved instrument LITOS (Leibniz Institute Turbulence Observations in the
Stratosphere) <xref ref-type="bibr" rid="bib1.bibx13" id="paren.8"/>, the energy dissipation rate <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula>
is obtained independent of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> by means of spectral analysis of wind
fluctuations. Thus it is possible to check the relation <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>∝</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.</p>
      <p>Please note that our comparison involves two parameters: (a) evaluation method
(Thorpe or spectral analysis) and (b) vertical resolution (low or high). We
concentrate on results from high-resolved spectral analysis (as a very precise
method of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> determination) and low-resolved Thorpe analysis. Such
a Thorpe evaluation of radiosonde data has been proposed for extensive use
<xref ref-type="bibr" rid="bib1.bibx2 bib1.bibx8" id="paren.9"/>. Note that <xref ref-type="bibr" rid="bib1.bibx8" id="normal.10"/>
call 1 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Hz</mml:mi></mml:math></inline-formula> (5 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>) high resolution, while we call it low resolution
(compared to LITOS with 8 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">kHz</mml:mi></mml:math></inline-formula>). In principle, the Thorpe analysis can
also be performed on data with higher resolution, as done, e.g., by
<xref ref-type="bibr" rid="bib1.bibx10" id="normal.11"/> for temperature data with a 50 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">Hz</mml:mi></mml:math></inline-formula> sampling rate; however,
these data are rarely available compared to those of standard radiosonde. Furthermore, a kind
of spectral analysis can be used to determine dissipation rates from
low-resolution wind data <xref ref-type="bibr" rid="bib1.bibx1" id="paren.12"/>, but this method depends on the
absolute value of the wind velocity, which is not available for our measurements
(see next section).</p>
      <p>In Sect. <xref ref-type="sec" rid="Ch1.S2"/>, the measurement principle of LITOS and the
determination of the energy dissipation rates with both methods are shortly
reviewed. The independent measurements of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are
compared in Sect. <xref ref-type="sec" rid="Ch1.S3"/>. Section <xref ref-type="sec" rid="Ch1.S4"/> shows results for
the energy dissipation rate <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> from both a Thorpe analysis and our
high-resolved spectral analysis. Conclusions are drawn in
Sect. <xref ref-type="sec" rid="Ch1.S5"/>.</p>
</sec>
<sec id="Ch1.S2">
  <title>Instrumentation and methods</title>
      <p>As described in <xref ref-type="bibr" rid="bib1.bibx13" id="normal.13"/>, LITOS is a balloon-borne instrument
which measures winds with high vertical resolution of millimetres. The wind
sensor is a constant temperature anemometer (CTA), which facilitates the cooling
effect on a heated wire of 5 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">µ</mml:mi><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> diameter. To infer wind velocities
from the anemometer voltage, a calibration in the same ambient conditions
(pressure, temperature) is required. This is not possible for a balloon flight,
as the pressure varies within several orders of magnitude during the flight.
Nevertheless, we are only interested in the spectral form, and the absolute
values are not important (see below); therefore we use the anemometer voltage
for the analysis. The vertical resolution is obtained by applying a sample rate
of 8 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">kHz</mml:mi></mml:math></inline-formula> with a balloon ascent rate of 5 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">m</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">s</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>.  To date,
three flights on large (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>10 000</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi mathvariant="normal">m</mml:mi><mml:mn mathvariant="normal">3</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>) balloons have been performed,
namely Balloon Experiments for University Students (BEXUS) 6, 8 and 12 in 2008,
2009 and 2011, respectively. They were launched at Kiruna
(68<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> N, 21<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> E) in autumn.
For BEXUS 6, the radiosonde data are partly disturbed so that it is not considered
in this article.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1" specific-use="star"><caption><p>
Example of raw data (left) and associated power spectrum (right) computed for
the shaded area in the raw data plot.
In the raw data, an amplitude of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">≲</mml:mi></mml:math></inline-formula> 1 mV corresponds to instrumental
noise. In the spectrum, the blue curve shows the measurement, the grey dashed
lines the 95 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> confidence interval and the red curve the fit of the
Heisenberg model to the measured spectrum; the red vertical line indicates the
inner scale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>. The green dashed lines display slopes of <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> and <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">7</mml:mn></mml:mrow></mml:math></inline-formula>.
The errors given are fit errors.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015-f01.pdf"/>

      </fig>

      <p>The left panel in Fig. <xref ref-type="fig" rid="Ch1.F1"/> shows an example of a time series of
the anemometer voltage of the BEXUS 12 flight. Large-scale motions have already
been removed by subtracting a spline. At altitudes with small variations
(<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">≲</mml:mi></mml:math></inline-formula> 1 mV, e.g. from 10.28 to 10.3 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>), the signal mainly
shows instrumental noise; this corresponds to a calm region. Large fluctuations,
as in the height range of 10.18 to 10.28 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, correspond to turbulence.
Note that there is a substructure which divides the turbulent region into
different patches.  For the patch from 10.27 to 10.28 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> (shaded in the
graph), the power spectral density (PSD) is plotted in the right panel of
Fig. <xref ref-type="fig" rid="Ch1.F1"/> (blue curve). An inertial regime with a <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 and
the transition to the viscous subrange with a <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">7</mml:mn></mml:mrow></mml:math></inline-formula> slope is identified. The part
below <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">2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> m spatial scale with approximately constant PSD
corresponds to the instrumental noise level. As the transition to the inertial
range is resolved, a fit of the <xref ref-type="bibr" rid="bib1.bibx6" id="text.14"/> model in the form given
by <xref ref-type="bibr" rid="bib1.bibx9" id="text.15"/> is applied to the experimental data (red curve). This
gives the inner scale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>, i.e. the transition from the inertial to the
viscous subrange. In the example, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:mn>1.9</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mi mathvariant="normal">m</mml:mi><mml:mo>±</mml:mo><mml:mn>4.5</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:mrow></mml:msup><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula> (fit error). Note that <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> does not depend on the
absolute value of the PSD, only on identifying the bend in the spectrum. From
the inner scale, the energy dissipation rate is obtained by

              <disp-formula id="Ch1.E3" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">4</mml:mn></mml:msup><mml:mfrac><mml:mrow><mml:msup><mml:mi mathvariant="italic">ν</mml:mi><mml:mn mathvariant="normal">3</mml:mn></mml:msup></mml:mrow><mml:mrow><mml:msubsup><mml:mi>l</mml:mi><mml:mn mathvariant="normal">0</mml:mn><mml:mn mathvariant="normal">4</mml:mn></mml:msubsup></mml:mrow></mml:mfrac><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>

        where <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ν</mml:mi></mml:math></inline-formula> is the kinematic viscosity (derived from the radiosonde measurement
of temperature and pressure on the same gondola), and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>c</mml:mi><mml:mo>=</mml:mo><mml:mn>5.7</mml:mn></mml:mrow></mml:math></inline-formula>
<xref ref-type="bibr" rid="bib1.bibx13 bib1.bibx5" id="paren.16"/>. For the example in Fig. <xref ref-type="fig" rid="Ch1.F1"/>,
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>=</mml:mo><mml:mn>3.2</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:msup><mml:mspace linebreak="nobreak" width="0.125em"/><mml:mi mathvariant="normal">W</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">kg</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> <inline-formula><mml:math display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mrow><mml:mn>3.0</mml:mn><mml:mo>×</mml:mo><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">4</mml:mn></mml:mrow></mml:msup><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mi mathvariant="normal">W</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">kg</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>.</p>
      <p>In order to obtain a vertical profile of energy dissipation rate, a sliding
window of 5 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">s</mml:mi></mml:math></inline-formula> (roughly 25 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> altitude) is used. For each window,
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> is computed according to the procedure described above. For
non-turbulent spectra, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> is set to 0.
A spectrum is regarded as non-turbulent if the noise-level detection fails,
if the inner scale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> is not within the fit range, if <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> has
implausible values (less than 0 or greater than 100 W 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>) or if the
mean distance between the fit and the data is larger than a fixed threshold. That
means the decision is made automatically based on a set of objective criteria.
The resulting <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> profile has a vertical resolution of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>10</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> due to the selected overlap.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2"><caption><p>
Potential temperature profile (left) and Thorpe displacement (right) for the
BEXUS 12 flight. The inset in the left panel shows a magnification from 15.48 to
15.80 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> for better visibility of instabilities (manifested as negative
gradients of potential temperature).</p></caption>
        <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015-f02.pdf"/>

      </fig>

      <p>The Thorpe analysis is performed similar to the procedure described in
<xref ref-type="bibr" rid="bib1.bibx19" id="normal.17"/> on data from a Vaisala RS92 radiosonde, which was on the same
gondola as the CTA sensors. Moisture is handled using the routine given
by <xref ref-type="bibr" rid="bib1.bibx20" id="normal.18"/>. To this end, saturated regions are detected, and a
composite potential temperature profile <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="normal">Θ</mml:mi><mml:mo>*</mml:mo></mml:msub></mml:mrow></mml:math></inline-formula> is computed by integration of
<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∂</mml:mo><mml:mi mathvariant="normal">Θ</mml:mi><mml:mo>/</mml:mo><mml:mo>∂</mml:mo><mml:mi>z</mml:mi></mml:mrow></mml:math></inline-formula> using the moist buoyancy frequency within those
saturated regions and the dry buoyancy frequency otherwise. The left panel of
Fig. <xref ref-type="fig" rid="Ch1.F2"/> shows the potential temperature profile for
the BEXUS 12 flight. In the inset, the part from 15.48 to
15.80 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> is magnified for better visibility of instabilities,
which manifest as negative gradients of potential temperature. The Thorpe
displacement is shown in the right panel of Fig. <xref ref-type="fig" rid="Ch1.F2"/>.  Large
displacements correspond to large vertical extents of unstable layers.  To
identify unstable layers and their vertical extension, the cumulative sum of the
Thorpe displacement (which is negative within an unstable region and 0 within
a stable one) is used. To select real overturns and discard negative potential
temperature gradients originating from measurement noise, a statistical test is
applied. To this end, the range of the potential temperatures within an
inversion is compared with the range of a pure noise sample of the same length <xref ref-type="bibr" rid="bib1.bibx18" id="paren.19"/>.
We assume here that the standard deviation of instrumental noise in segments of
200 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> is described by half the square of the standard deviation of
first differences of the potential temperature after trend removal.
For each detected unstable layer, the Thorpe length is computed according to
Eq. (<xref ref-type="disp-formula" rid="Ch1.E1"/>).</p>
      <p>Only significant overturns with a 99 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> percentile are used, discarding
<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>45</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> (BEXUS 8) and <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>30</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> (BEXUS 12)
of the inversions as noise-induced. The mean trend-to-noise ratio
(TNR) is <inline-formula><mml:math display="inline"><mml:mrow><mml:mover accent="true"><mml:mi mathvariant="italic">ξ</mml:mi><mml:mo mathvariant="normal">¯</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:mn>1.7</mml:mn></mml:mrow></mml:math></inline-formula> for the BEXUS 8 flight and <inline-formula><mml:math display="inline"><mml:mrow><mml:mover accent="true"><mml:mi mathvariant="italic">ξ</mml:mi><mml:mo mathvariant="normal">¯</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:mn>4.1</mml:mn></mml:mrow></mml:math></inline-formula> for the
BEXUS 12 flight.</p>
      <p>Several thin layers of only 10 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> or 20 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> passed the
significance test. We are aware that this is on the edge of radiosonde
capability.
These thin layers would to a large extent be suppressed if the instrument noise
were set to the standard deviation of first differences divided by
<inline-formula><mml:math display="inline"><mml:msqrt><mml:mn mathvariant="normal">2</mml:mn></mml:msqrt></mml:math></inline-formula> as done by <xref ref-type="bibr" rid="bib1.bibx19" id="text.20"/>.
However, LITOS also shows many thin layers.
Hence, this procedure would result in many fewer coincident layers especially in the stratosphere and,
by this, bias the comparison.
Nevertheless, as we will describe below, our main results are independent from the procedure of noise calculation.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3"><caption><p>
Thorpe length (left) and Ozmidov scale (right) vs. altitude for the detected
inversions of the BEXUS 12 flight. In the right panel, the cyan curve shows the Ozmidov scale
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> in the full resolution of the LITOS profile, the blue bars visualise
averages over the inversions detected by the radiosonde (<inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula>).</p></caption>
        <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015-f03.pdf"/>

      </fig>

</sec>
<sec id="Ch1.S3">
  <title>Comparison of Thorpe and Ozmidov scales</title>
      <p>A plot of the Thorpe length for the BEXUS 12 flight is shown in the left panel
of Fig. <xref ref-type="fig" rid="Ch1.F3"/>.  Unstable layers take up
50 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> of the altitude and can be found in the whole range. Large
Thorpe lengths stand out, e.g., at 5 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, between 5 and
10 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> and near 25 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> altitude, corresponding to the large
values of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>D</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> in the right panel of Fig. <xref ref-type="fig" rid="Ch1.F2"/>. Mean
values of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are 29 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> in the troposphere and
22 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> in the stratosphere; i.e. the Thorpe length is slightly
larger in the less stable troposphere.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4"><caption><p>
Zoomed plot of Thorpe (green) and Ozmidov (cyan) scales for the BEXUS 12 flight.
The potential temperature is plotted in red.</p></caption>
        <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015-f04.pdf"/>

      </fig>

      <p>The Ozmidov scale is computed from the energy dissipation rate obtained by
LITOS, using Eq. (<xref ref-type="disp-formula" rid="Ch1.E2"/>) and <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">α</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula>.  The
Brunt–Väisälä frequency <inline-formula><mml:math display="inline"><mml:mi>N</mml:mi></mml:math></inline-formula> is calculated from the radiosonde data as it
only slowly varies with altitude. In that computation, the sorted potential
temperature profile is used instead of the original data, because a background
stratification is needed and an imaginary <inline-formula><mml:math display="inline"><mml:mi>N</mml:mi></mml:math></inline-formula> should be avoided
<xref ref-type="bibr" rid="bib1.bibx3" id="paren.21"><named-content content-type="post">Sect. 3</named-content></xref>.  The result for the BEXUS 12 flight is plotted in
the right panel of Fig. <xref ref-type="fig" rid="Ch1.F3"/> (cyan curve).  According to
LITOS, 53 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> of the atmosphere is turbulent, i.e. <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>&gt;</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>
and hence <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>&gt;</mml:mo><mml:mn mathvariant="normal">0</mml:mn></mml:mrow></mml:math></inline-formula>.</p>
      <p>Figure <xref ref-type="fig" rid="Ch1.F4"/> shows the Thorpe length and the Ozmidov scale for
the altitude range of 15.48 to 15.80 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>. As LITOS
computes <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> on a constant grid independent of the layers, the
substructure of larger turbulent layers can be seen (e.g. from <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>15.5</mml:mn></mml:mrow></mml:math></inline-formula> to 15.62 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>), while the Thorpe length is a
per-layer value by construction.
From 15.706 to 15.789 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>, only LITOS observes turbulence while the
Thorpe method does not. The decrease of potential temperature
is not significant, so the Thorpe method is blind for the
turbulent motions.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5"><caption><p>
Thorpe scale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> vs. Ozmidov scale <inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula>
for the BEXUS 8 (green) and 12 (magenta) flights.
The black diagonal line represents <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.
The histograms show the distributions of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>,
respectively, of the composite data set of BEXUS 8 and BEXUS 12, i.e. of
all data points in the graph.
The occurrence axes have a linear scale and are omitted for readability.
Note that <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is limited by the resolution of the radiosonde
(<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>10</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>).</p></caption>
        <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015-f05.pdf"/>

      </fig>

      <p>In order to do a comparison between both length scales, the layers where both
methods detect turbulence are selected. For BEXUS 8 (BEXUS 12),
86 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> (69 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula>) of the significant, unstable layers are also
detected by LITOS, and 90 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> (88 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula>) of the layers detected by
LITOS intersect with a significant, unstable layer. The energy dissipation rate
(obtained from LITOS) is averaged over the layer (as detected by the Thorpe
analysis of radiosonde data). Such mean values over a Thorpe layer will be
denoted by averaging brackets <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mo>⋅</mml:mo><mml:mo>〉</mml:mo></mml:mrow></mml:math></inline-formula>. For each unstable layer,
the resulting <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>〉</mml:mo></mml:mrow></mml:math></inline-formula> is plugged into
Eq. (<xref ref-type="disp-formula" rid="Ch1.E2"/>) to infer an Ozmidov scale
<inline-formula><mml:math display="inline"><mml:mrow><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>=</mml:mo><mml:msqrt><mml:mrow><mml:mo>〈</mml:mo><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>〉</mml:mo><mml:mo>/</mml:mo><mml:mo>〈</mml:mo><mml:mi>N</mml:mi><mml:msup><mml:mo>〉</mml:mo><mml:mn mathvariant="normal">3</mml:mn></mml:msup></mml:mrow></mml:msqrt></mml:mrow></mml:math></inline-formula> for the layer. The blue bar plot in the right panel of
Fig. <xref ref-type="fig" rid="Ch1.F3"/> shows a graph for the BEXUS 12 flight.  The
layer near 5 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> with large <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, e.g., is also seen in
<inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula>, albeit less pronounced. In contrast, at
<inline-formula><mml:math display="inline"><mml:mo>∼</mml:mo></mml:math></inline-formula>10 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> altitude the Ozmidov scale is larger than the Thorpe scale.
Mean values of <inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> are 15 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> in the
troposphere and 6 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula> (i.e. only half the value) in the stratosphere.
Thus, in qualitative agreement with Eq. (<xref ref-type="disp-formula" rid="Ch1.E2"/>), the less
stable troposphere shows on average a larger Ozmidov scale, i.e. larger
eddies. As the Thorpe length shows similar behaviour (see above), this
generally supports the assumption of a relation between <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>.</p>
      <p>In Fig. <xref ref-type="fig" rid="Ch1.F5"/> Ozmidov scale <inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> and Thorpe
length <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are plotted against each other for those 136
(175) significant, unstable layers of the BEXUS 8 (BEXUS 12) flight where
turbulence has been detected by LITOS. Both length scales are of the same order
of magnitude, but no direct relation between them can be seen in either flight.
The correlation coefficient between both is 0.32 for BEXUS 8 and 0.33 for
BEXUS 12. Note that <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is limited by the resolution of the
radiosonde (<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>10</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>).
An analogous plot for the simultaneous layers obtained using the more
restrictive noise estimation of <xref ref-type="bibr" rid="bib1.bibx19" id="normal.22"/> contains similar scatter with
no apparent correlation.</p>
      <p>The histograms in the top and in the right axes in Fig. <xref ref-type="fig" rid="Ch1.F5"/> show the
distributions for <inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, respectively,
for the composite dataset of BEXUS 8 and BEXUS 12. The maximum for the Thorpe
length is slightly larger than for the Ozmidov scale. The decrease towards large
scales is similar for both lengths. At small scales <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is limited by
the resolution of the radiosonde which produces the cut-off at 10 m, while the
histogram for <inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> shows a continuous decrease.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6"><caption><p>
Statistics for the ratio <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>/</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> for the
BEXUS 8 (top) and BEXUS 12 (bottom) flights.
The red curves show the most likely normal distributions for the logarithmic data.</p></caption>
        <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015-f06.pdf"/>

      </fig>

      <p>In contrast to our measurements, an approximate proportionality between Thorpe
and Ozmidov lengths is observed in the ocean
<xref ref-type="bibr" rid="bib1.bibx3 bib1.bibx16 bib1.bibx15" id="paren.23"><named-content content-type="pre">e.g.</named-content></xref>.  For example,
<xref ref-type="bibr" rid="bib1.bibx16" id="normal.24"/> find that most of their data fall between <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mo>(</mml:mo><mml:mn mathvariant="normal">1</mml:mn><mml:mo>/</mml:mo><mml:mn mathvariant="normal">4</mml:mn><mml:mo>)</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, with a range from
<inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mn>10</mml:mn><mml:mrow><mml:mo>-</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:msup></mml:mrow></mml:math></inline-formula> m to <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mn>10</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>.  This is the basis for applying the Thorpe
analysis on atmospheric data.  Several authors
<xref ref-type="bibr" rid="bib1.bibx4 bib1.bibx2 bib1.bibx7" id="paren.25"><named-content content-type="pre">e.g.</named-content></xref> have inferred
energy dissipation rates from the Thorpe analysis by plugging <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mi>c</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> into Eq. (<xref ref-type="disp-formula" rid="Ch1.E2"/>) and solving for
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula>, thus getting

              <disp-formula id="Ch1.E4" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>=</mml:mo><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msubsup><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi>N</mml:mi><mml:mn mathvariant="normal">3</mml:mn></mml:msup><mml:mo>.</mml:mo></mml:mrow></mml:math></disp-formula>

        Knowledge about the constant <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> is very limited (see discussion below), and
only <xref ref-type="bibr" rid="bib1.bibx4" id="normal.26"/> provide some information based on stratospheric data.
With our high-resolved wind data we can determine this constant independently.
<xref ref-type="bibr" rid="bib1.bibx17" id="normal.27"/> found the distribution of the ratio <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> to be lognormal,
which implies <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> to be lognormal as well.
Logarithmic histograms of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>/</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> for
the BEXUS 8 and BEXUS 12 flights are presented in Fig. <xref ref-type="fig" rid="Ch1.F6"/>.
The red curves display the most likely normal distributions for the logarithmic
data. They show a sufficient agreement to the histograms and are both centred around
<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>0.1</mml:mn></mml:mrow></mml:math></inline-formula>. The distribution of values is fairly
broad: the full width at half maximum (FWHM) spans <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>1.9</mml:mn></mml:mrow></mml:math></inline-formula> orders of magnitude.</p>
      <p>We have calculated the same histograms also for the layers that are extracted
using the more restrictive noise estimation of <xref ref-type="bibr" rid="bib1.bibx19" id="normal.28"/>. Even if here
only 36 (15) coincident layers are detected for BEXUS 8 (BEXUS 12), the
distribution of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> is of similar width. The most
probable values are slightly lower but agree within the uncertainty given by
the distribution of the data.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F7"><caption><p>
Energy dissipation rates from Thorpe analysis of the radiosonde (left) and
spectral analysis of the high-resolved wind measurement (right) for the BEXUS 12
flight. In the right panel, the cyan curve shows <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> in the full resolution, the
blue bars visualise averages over the unstable layers detected by the Thorpe analysis
(<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>〉</mml:mo></mml:mrow></mml:math></inline-formula>).</p></caption>
        <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015-f07.pdf"/>

      </fig>

</sec>
<sec id="Ch1.S4">
  <title>Energy dissipation rates</title>
      <p>The relation between the energy dissipation rate <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> and the length
scales discussed above involves the Brunt–Väisälä frequency; see
Eqs. (<xref ref-type="disp-formula" rid="Ch1.E2"/>) and (<xref ref-type="disp-formula" rid="Ch1.E4"/>). Thus the
<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> values computed from LITOS via spectral analysis and the ones from
the radiosonde via Thorpe analysis have to be compared separately.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8"><caption><p>
Ratio between energy dissipation rates from spectral analysis and from Thorpe
analysis for the significant, unstable layers of the BEXUS 12 flight.</p></caption>
        <?xmltex \igopts{width=236.157874pt}?><graphic xlink:href="https://www.atmos-chem-phys.net/15/2159/2015/acp-15-2159-2015-f08.pdf"/>

      </fig>

      <p>The left panel of Fig. <xref ref-type="fig" rid="Ch1.F7"/> shows an altitude profile of energy
dissipation rates obtained from the Thorpe analysis of the radiosonde on
BEXUS 12, assuming <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mi>c</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> with <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:mn>0.3</mml:mn></mml:mrow></mml:math></inline-formula> as in
<xref ref-type="bibr" rid="bib1.bibx2" id="normal.29"/>. In the right panel, the altitude profile of energy
dissipation obtained from LITOS is plotted in cyan, while the blue bars depict
the mean values <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>〉</mml:mo></mml:mrow></mml:math></inline-formula> over the unstable layers
detected by the Thorpe analysis, for comparability.  On average, the values are
of the same order of magnitude, and the profiles have a similar structure. The
large dissipation near <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>10</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula> in the CTA data does not stand out
in the Thorpe analysis.  The mean value over all significant, unstable
layers from Thorpe, 1 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">mW</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">kg</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>, is larger than the one from LITOS,
0.3 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">mW</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">kg</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>. For BEXUS 8 the averages are
3 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">mW</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">kg</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> from Thorpe and 2 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">mW</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">kg</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> from LITOS.
That fits the fact that the used value for <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>, 0.3, is larger than the one
obtained from our own data, <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:mn>0.1</mml:mn></mml:mrow></mml:math></inline-formula> (cf. Fig. <xref ref-type="fig" rid="Ch1.F6"/>).
If the whole <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> profile (not only the unstable layers detected by Thorpe)
is taken into account, the average dissipation rate obtained by LITOS is
0.4 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">mW</mml:mi><mml:mspace width="0.125em" linebreak="nobreak"/><mml:msup><mml:mi mathvariant="normal">kg</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> for BEXUS 12 and 2 <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">mW</mml:mi><mml:mspace linebreak="nobreak" width="0.125em"/><mml:msup><mml:mi mathvariant="normal">kg</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> for BEXUS 8.  To
get a closer look, the deviation of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:mi mathvariant="italic">ε</mml:mi><mml:mo>〉</mml:mo></mml:mrow></mml:math></inline-formula> from LITOS
to <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> inferred from the Thorpe analysis indicated by the ratio
<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mtext>LITOS</mml:mtext></mml:msub><mml:mo>〉</mml:mo><mml:mo>/</mml:mo><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mtext>Thorpe</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula>
of the blue and green curves in Fig. <xref ref-type="fig" rid="Ch1.F7"/> is plotted in
Fig. <xref ref-type="fig" rid="Ch1.F8"/>. It reveals a large range of 5
orders of magnitude. Overall, for 71 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> (BEXUS 8: 64 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula>)
of the layers, <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> inferred from the Thorpe analysis is larger than
the value from the spectral analysis. That the ratio is sometimes larger and
sometimes smaller than unity illustrates that the most likely value of <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> does
not contain the whole information, but the width of the distribution is important.
The correlation coefficient between <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>〈</mml:mo><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mtext>LITOS</mml:mtext></mml:msub><mml:mo>〉</mml:mo></mml:mrow></mml:math></inline-formula>
and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi mathvariant="italic">ε</mml:mi><mml:mtext>Thorpe</mml:mtext></mml:msub></mml:mrow></mml:math></inline-formula> is 0.06 (BEXUS 8: 0.39). Due to the influence of the
Brunt–Väisälä frequency, pronounced peaks in <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> or
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> (Fig. <xref ref-type="fig" rid="Ch1.F3"/>) do not necessarily correspond
to large <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> (Fig. <xref ref-type="fig" rid="Ch1.F7"/>), e.g. at <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">5</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">km</mml:mi></mml:math></inline-formula>.</p>
</sec>
<sec id="Ch1.S5" sec-type="conclusions">
  <title>Discussion and conclusions</title>
      <p>In this paper, the first extensive examination of the relation between the
Thorpe length <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and Ozmidov scale <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> for stratospheric
conditions was performed, using the new high-resolution instrument LITOS and
a radiosonde on the same gondola. Therewith, the assumption for computing
energy dissipation rates <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> from a Thorpe analysis of standard
radiosondes, namely the proportionality <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>∝</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>, was
checked. In our data no obvious relation between <inline-formula><mml:math display="inline"><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover></mml:math></inline-formula> and
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> can be seen, particularly no proportionality.  The
proportionality “constant” used in radiosonde analyses, <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:mo>(</mml:mo><mml:mover accent="true"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow><mml:mo mathvariant="normal">‾</mml:mo></mml:mover><mml:mo>/</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula>, shows a very broad distribution with
a width of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:math></inline-formula> orders of magnitude. This is also reflected in the large
deviation of <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula> values up to a factor of <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn>3000</mml:mn></mml:mrow></mml:math></inline-formula> obtained with
both methods.  Nevertheless, although the values for individual layers are
highly variable, the mean of <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> is 0.1 for both BEXUS 12 and BEXUS 8,
which is close to 0.3 used by <xref ref-type="bibr" rid="bib1.bibx2" id="normal.30"/>, who
reviewed oceanic measurements to obtain that value. <xref ref-type="bibr" rid="bib1.bibx7" id="normal.31"/>
obtained <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:mn>1.0</mml:mn></mml:mrow></mml:math></inline-formula> by a comparison of radiosonde data to radar measurements.
<xref ref-type="bibr" rid="bib1.bibx4" id="normal.32"/> used <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>=</mml:mo><mml:mn>1.32</mml:mn></mml:mrow></mml:math></inline-formula> (<inline-formula><mml:math display="inline"><mml:mrow><mml:mi>c</mml:mi><mml:mo>=</mml:mo><mml:mn>1.15</mml:mn></mml:mrow></mml:math></inline-formula>) referring to a French
thesis; this value was obtained from selected thick stratospheric layers
(<inline-formula><mml:math display="inline"><mml:mrow><mml:mo>&gt;</mml:mo><mml:mn>200</mml:mn><mml:mspace width="0.125em" linebreak="nobreak"/><mml:mi mathvariant="normal">m</mml:mi></mml:mrow></mml:math></inline-formula>) with statistically homogeneous turbulence. However, in those
publications no data basis, distribution width or error is given. Recently,
<xref ref-type="bibr" rid="bib1.bibx21" id="normal.33"/> reported a few case studies of turbulent layers in the
troposphere detected simultaneously by radar and balloon; using their reported
estimates of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> leads to values of <inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:math></inline-formula> between
0.1 and 1.6.</p>
      <p>One reason for discrepancies from the proportionality <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>∝</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> may be that large overturns might change significantly during the
time the sensor needs to fly through the layer, such that the sorting procedure
then no longer makes sense. Furthermore, direct numerical simulations by
<xref ref-type="bibr" rid="bib1.bibx12" id="normal.34"/> indicate that <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">O</mml:mi></mml:msub><mml:mo>/</mml:mo><mml:msub><mml:mi>L</mml:mi><mml:mi mathvariant="normal">T</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is not constant
but rather depends on the age of turbulence.</p>
      <p>Some turbulent layers are not detected at all by the Thorpe analysis. Those are
not associated with a (significant) negative gradient of potential temperature,
which is necessary for detection by the Thorpe method. Not all turbulence is
related to static instabilities. Even if initially a negative
potential temperature gradient may have occurred, it is removed by the
turbulent motions which outlive the instability; such fossil turbulence
cannot be detected by the Thorpe method. Apart from that, turbulent layers may
be too thin to be observed with the relatively coarse vertical resolution of the
radiosonde. On the other hand, some unstable layers detected by the Thorpe
analysis are not observed by LITOS. An explanation is that the static
instability may not yet have led to turbulent motions. In these cases,
a correspondence between both measurements is not expected.</p>
      <p>Not all layers are detected by both systems. Of the significant layers
detected by the Thorpe analysis, 86 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> (BEXUS 8) and 69 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula>
(BEXUS 12) are also detected by LITOS. For BEXUS 12, the mean thickness of
significant, unstable layers as detected by the Thorpe analysis is 53 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>.
The mean thickness of those significant layers also detected by LITOS is
63 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>; that of significant layers not detected by LITOS is only
31 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">m</mml:mi></mml:math></inline-formula>.
That means that the simultaneous detection depends on the size of the layer;
mainly thin layers are detected by only one method. But as this only applies to
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="italic">≲</mml:mi><mml:mn>30</mml:mn></mml:mrow></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">%</mml:mi></mml:math></inline-formula> of the layers, and those layers were taken out of the
comparison, the bias for our results should be small.</p>
      <p>For LITOS, the detection limit for <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> on small scales (i.e. high
frequencies or large <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula>) is given by the sampling rate. This limit
has been encountered in a few cases for small regions where the inertial range
extends further than the Nyquist limit of 4 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">kHz</mml:mi></mml:math></inline-formula>. For large scales
(i.e. low frequencies or small <inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">ε</mml:mi></mml:math></inline-formula>), the detection limit is
determined by the trend removal and the window length. As a
reasonable part of the inertial range has to be resolved to enable a fit, the
limit is estimated to <inline-formula><mml:math display="inline"><mml:mrow><mml:mo>∼</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow></mml:math></inline-formula> m. The maximal identified <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>l</mml:mi><mml:mn mathvariant="normal">0</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> values
of 10 cm and 8.7 cm for BEXUS 8 and BEXUS 12, respectively, were
far below this limit. That means that these limitations do not
affect the results.</p>
      <p>To date, we have only two flights with data usable for the
analysis presented in this paper, namely BEXUS 8 and BEXUS 12,
which both took place at polar latitudes near autumn equinox. Of
course they cannot represent the whole variability of the
stratosphere. Nevertheless, although there are differences between
both flights, such as dissipation rates being on average 1 order
of magnitude higher for BEXUS 8, these are not relevant for the
results discussed above.  More flights with our new high-resolution
instrument are planned to broaden the data basis.</p>
      <p>Our results question the applicability of the Thorpe analysis for
the extraction of energy dissipation rates for individual turbulent
layers. Nevertheless, statements in the statistical mean seem to be
possible.
Further research on the relation between Thorpe and Ozmidov lengths
and the temporal evolution of turbulence is necessary.</p>
</sec>

      
      </body>
    <back><ack><title>Acknowledgements</title><p>The data from the BEXUS 8 flight were kindly provided by Anne Haack.
The BEXUS programme was financed by the German Aerospace Center
(DLR) and the Swedish National Space Board (SNSB).  We are grateful
for the support by the “International Leibniz Graduate School for
Gravity Waves and Turbulence in the Atmosphere and Ocean” (ILWAO)
funded by the Leibniz Association (WGL).
Furthermore, we would like to thank Lars Umlauf for helpful discussions.
We thank the reviewers Richard Wilson and Marvin Geller for their helpful comments.<?xmltex \hack{\newline}?><?xmltex \hack{\newline}?>
Edited by: W. Ward<?xmltex \hack{\newline}?></p></ack><?xmltex \hack{\newpage}?><?xmltex \hack{\newpage}?><ref-list>
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