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  <front>
    <journal-meta>
<journal-id journal-id-type="publisher">JSSS</journal-id>
<journal-title-group>
<journal-title>Journal of Sensors and Sensor Systems</journal-title>
<abbrev-journal-title abbrev-type="publisher">JSSS</abbrev-journal-title>
<abbrev-journal-title abbrev-type="nlm-ta">J. Sens. Sens. Syst.</abbrev-journal-title>
</journal-title-group>
<issn pub-type="epub">2194-878X</issn>
<publisher><publisher-name>Copernicus Publications</publisher-name>
<publisher-loc>Göttingen, Germany</publisher-loc>
</publisher>
</journal-meta>

    <article-meta>
      <article-id pub-id-type="doi">10.5194/jsss-5-373-2016</article-id><title-group><article-title>Annular arrays for novel ultrasonic <?xmltex \hack{\break}?> measurement techniques</article-title>
      </title-group><?xmltex \runningtitle{Annular arrays for novel ultrasonic measurement techniques}?><?xmltex \runningauthor{M.~Wolf et al.}?>
      <contrib-group>
        <contrib contrib-type="author" corresp="yes" rid="aff1">
          <name><surname>Wolf</surname><given-names>Mario</given-names></name>
          <email>mario.wolf@tu-dresden.de</email>
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Kühnicke</surname><given-names>Elfgard</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Kümmritz</surname><given-names>Sebastian</given-names></name>
          
        </contrib>
        <contrib contrib-type="author" corresp="no" rid="aff1">
          <name><surname>Lenz</surname><given-names>Michael</given-names></name>
          
        </contrib>
        <aff id="aff1"><institution>Solid-State Electronics Laboratory, Dresden University of
Technology, Dresden, Germany</institution>
        </aff>
      </contrib-group>
      <author-notes><corresp id="corr1">Mario Wolf (mario.wolf@tu-dresden.de)</corresp></author-notes><pub-date><day>1</day><month>November</month><year>2016</year></pub-date>
      
      <volume>5</volume>
      <issue>2</issue>
      <fpage>373</fpage><lpage>380</lpage>
      <history>
        <date date-type="received"><day>29</day><month>April</month><year>2016</year></date>
           <date date-type="rev-recd"><day>30</day><month>August</month><year>2016</year></date>
           <date date-type="accepted"><day>22</day><month>September</month><year>2016</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://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016.html">This article is available from https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016.html</self-uri>
<self-uri xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016.pdf">The full text article is available as a PDF file from https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016.pdf</self-uri>


      <abstract>
    <p>The paper shows how the precise knowledge of the sound field of an
ultrasonic annular array can contribute to the development of novel
measurement techniques. Emphasis is placed on (a) a non-invasive method for
sound velocity measurements in fluids using the echo signals from scattering
p]articles, (b) a non-invasive method for the combined determination of
thickness and sound velocity in layered structures by using a novel focusing
technique, and (c) a non-scanning curvature measurement method exploiting the
wave front curvature of a reflected wave. To demonstrate the methods, the
principles as well as results of simulations and measurements are discussed.</p>
  </abstract>
    </article-meta>
  </front>
<body>
      

<sec id="Ch1.S1" sec-type="intro">
  <title>Introduction</title>
      <p>Conventional ultrasonic pulse-echo methods measure the time of flight (ToF)
as the only quantity. This is used to determine the sound velocity or the
distance of a reflector, while the other quantity has to be known. For
imaging in non-destructive testing (NDT) or in medical diagnostics, the
value of sound velocity is assumed a priori. Interfaces of hidden objects
are imaged by the measured ToF. The supposed locations and dimension of
these objects are incorrect if the actual sound velocity differs from the
assumed one. For material characterization, the thickness of a specimen is
determined by mechanical measurements and the sound velocity is determined
by ToF measurements. For multi-layered structures the mechanical or optical
determination of the thickness of the different layers is impossible
non-destructively. It is necessary to determine both quantities
simultaneously to get information about the thickness and the material of
the different layers.</p>
      <p>To measure sound velocity locally resolved by means of tomography, usually a
high number of reflectors or transducers at known positions are required
(Huang et al., 2004) and the test object has to be accessible from all
directions. A method for the simultaneous measurement of thickness and sound
velocity for a single-layer specimen with coplanar surfaces is introduced by
Hsu et al. (1992) and Dayal (1992) and pursued by Kim et al. (2003). For that
method, the specimen has to be placed in a medium with a known sound
velocity and between two probes with a known distance. The ToFs of
different reflected and transmitted signals are evaluated to determine the
thickness and sound velocity of the plate. Such an invasive method is
suitable for small and not embedded components and is qualified only for an
one-layered specimen. Loosvelt and Lasaygues (2011) use this method for plates with
a thickness smaller than the wavelength.</p>
      <p>This paper demonstrates how additional information of the reflected sound
field is gathered by using segmented annular arrays. New measurement
techniques have been developed, being characterized by a close combination
of sound field simulations and measurements. They use synthetic or
electronic focusing and analyse the phases and amplitudes on all transducer
elements to determine the object curvature radius or sound velocity and
distance simultaneously. These approaches require the precise knowledge of
the sound field dependent on the array parameters and the set-up.
Therefore, sound field simulations are necessary.</p>
      <p>A half-analytical method has been developed to optimize transducers and to
calculate the sound field in complex structures and layered media. It is
based on time-harmonic Green's functions in a steepest descent approximation
for a two-dimensional geometry. The source area is discretized and uniformly
covered with point sources. The sound field that is irradiated from a
finitely extended source is the superposition of the field of all point
sources. The sound field in a layered medium can be calculated approximately
by a decomposition of the medium into different layers and a separate
calculation of wave propagation in each layer (Kühnicke, 2007). This
method is applied for each element to simulate the field generated in the
medium or at the different interfaces, including the reflections back to the
transducer. The applied focusing techniques can be realized by phase
shifting and superposing the different fields.</p>
      <p>Different annular arrays are used (Fig. 1). They have six active ring
elements and, depending on the task, a curved interface for a small focus
extension or additional segments for non-axis-symmetric problems or
adjustment (Fig. 1, right). The centre frequencies are between 3  and
10 MHz, and the central elements have diameters from 4  to 5 mm with
results in near-field lengths between 10  and 30 mm. The outer rings have
the same area and so the same near-field length, which enables a well
focusing. The active material is a composite made by the dice and fill
technique (Janas and Safari,  1995).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F1"><caption><p>Geometry of the annular arrays: the numbering used in the
following paragraphs starts at one for the central element and ends with six
for the fifth ring; e.g. <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mn>16</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> is the signal emitted from the central
element and received at the fifth ring.</p></caption>
        <?xmltex \igopts{width=199.169291pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f01.png"/>

      </fig>

</sec>
<sec id="Ch1.S2">
  <title>Scattering particle method for locally resolved measurement of sound
velocity</title>
      <p>The monitoring of sound velocity is of great interest in chemical processes
because sound velocity is a measure for concentration, mass density and
elastic parameters. Other possible applications of locally resolved sound
velocity measurements are tissue characterization and noninvasive
temperature monitoring during hyperthermia for cancer therapy.</p>
      <p>Conventional pulse-echo methods measure the ToF to determine only
one quantity: the sound velocity or the distance of a reflector. However, the
other quantity has to be known. To measure a local distribution of sound
velocity, usually further reflectors or transducers at known positions are
required. These additional mechanical parts cause a high instrumentation
effort. If the examined medium is not all-round accessible, transducers/reflectors have to be inserted, which can affect the examined process.
Therefore, a non-invasive method without the need for fixed reflectors is
most desirable to measure sound velocity profiles.</p>
      <p>This paper presents a novel approach for simultaneous measurement of sound
velocities and distances in fluids containing moving scattering particles.
Because the sound field of an ultrasonic transducer depends on both the
transducer parameters and the sound velocity of the propagation medium, the
focus position is used as a second measuring quantity instead of using only
the propagation time. The focus position is determined by evaluating the
echoes of the scatterers. The echo of a single particle becomes strongest if
it is located in the focal zone of the sound field. Because particles are in
motion in a fluid, it is possible to assume a uniform distribution of
particles in time average. So the averaged amplitude of echo signals becomes
maximal for the ToF to the focus and back (Fig. 2).</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F2"><caption><p>Normalized amplitude of averaged echo signals of an annular array
at focusing <italic>Fok</italic> <inline-formula><mml:math display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> 40 mm in water of 30 <inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula>C (<inline-formula><mml:math display="inline"><mml:mi>c</mml:mi></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> 1510 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>) for
different numbers of averages (Maximum at <inline-formula><mml:math display="inline"><mml:mi>t</mml:mi></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> 52 <inline-formula><mml:math display="inline"><mml:mi mathvariant="normal">µ</mml:mi></mml:math></inline-formula>s).</p></caption>
        <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f02.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F3"><caption><p>Calculated sound fields (focusing in send and receive mode) dependent on the sound velocity in the propagation medium for a curved
9 MHz annular array at different control modes <italic>Fok</italic>.</p></caption>
        <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f03.png"/>

      </fig>

      <p>Lenz et al. (2011) and Lenz and Kühnicke (2012)  give proof of concept by measurements in fluids
covering a wide range of sound velocities with a strongly focusing
transducer equipped with a lens. An uncertainty in velocity determination of
less than 0.1 % was achieved in a detailed measurement using water at
different temperatures.</p>

      <?xmltex \floatpos{t}?><fig id="Ch1.F4" specific-use="star"><caption><p>Left: calibration curve – time of flight as a function of sound
velocity for different control modes; right: time of flight as a function of control mode for different sound velocities.</p></caption>
        <?xmltex \igopts{width=384.112205pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f04.png"/>

      </fig>

      <p>To achieve a local resolution of the sound velocity measurement along the
axis without additional mechanical effort, an ultrasonic array is required.
Due to the available electronic instrumentation, first measurements were
done by emission with one element and synthetic focusing of the received
signals, which means that signals are time shifted and superposed
(Kühnicke et al., 2011). The development of a new pulser allows driving
all elements together, whereby each pulse can be delayed with a definite
time lag. For a second focusing, the received signals are superposed and
thus focused synthetically. This reduces the statistical uncertainty
because it minimizes the focus extension and contributes to a larger signal-to-noise ratio.</p>
      <p>The control mode <italic>Fok</italic> corresponds to a set of delay times. The delay times are
chosen in such a way that the focus of the transducer is located at the
distance <inline-formula><mml:math display="inline"><mml:mrow><mml:mi>z</mml:mi><mml:mo>=</mml:mo></mml:mrow></mml:math></inline-formula> <italic>Fok</italic> in the calibration medium water at room temperature. This set
of delay times is used for all measurements, independently from the real
sound velocity.</p>
      <p>Because the focus position depends on the sound velocity of the medium,
sound field simulations are required to predict the focus position as a
function of the sound velocity of the medium, where the parameters of the
array need to be considered, as well. Figure 3 shows calculated sound fields
of the used curved annular array for two different control modes and for two
different sound velocities of the propagation medium.</p>
      <p>Figure 3 confirms that the focus position depends on the velocity of the
propagation medium (compare Fig. 3a with b, and c with d). The position
of the sound field maximum can be varied by means of control mode (compare
Fig. 3a with c, and b with d).</p>
      <p>To create calibration curves, the sound fields are simulated for different
sound velocities (and different control modes). The positions of the sound
field maxima are then converted into the corresponding ToFs.
Plotting the ToFs as a function of sound velocity for several
control modes <italic>Fok</italic> leads to the series of calibration curves depicted in Fig. 4.
Using the measured ToF in an unknown fluid and considering the
used control mode <italic>Fok</italic> then enables one to read off the sound velocity of the medium
using Fig. 4, left.</p>
      <p>To compare measurements and simulations, echoes of scattering particles and
therefore sound velocities and focus positions are measured in media with constant
temperature (Fig. 4, right). It is striking that the measured curves fit very
well to the simulations.</p>
      <p>The method has been qualified for media with constant sound velocity, and
for these measurements, an accuracy of more than 99.8 % was reached (Wolf
et al., 2013). It had been shown that the measurement uncertainty for
constant sound velocities can be reduced to 2.5 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>, which is less than
2 ‰, in water (see Table 1).</p>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T1"><caption><p>Reachable uncertainty.</p></caption><oasis:table frame="topbot"><?xmltex \begin{scaleboxenv}{.97}[.97]?><oasis:tgroup cols="3">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="left"/>
     <oasis:colspec colnum="3" colname="col3" align="left"/>
     <oasis:thead>
       <oasis:row>  
         <oasis:entry colname="col1">Number of</oasis:entry>  
         <oasis:entry colname="col2">Standard deviation <inline-formula><mml:math display="inline"><mml:mo>±</mml:mo></mml:math></inline-formula> 3<inline-formula><mml:math display="inline"><mml:mi mathvariant="italic">σ</mml:mi></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col3">Absolute error</oasis:entry>
       </oasis:row>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1">averaged signals</oasis:entry>  
         <oasis:entry colname="col2">of time of flight</oasis:entry>  
         <oasis:entry colname="col3">of sound velocity</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1">50</oasis:entry>  
         <oasis:entry colname="col2">500 ns</oasis:entry>  
         <oasis:entry colname="col3">13 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></oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">200</oasis:entry>  
         <oasis:entry colname="col2">250 ns</oasis:entry>  
         <oasis:entry colname="col3">6 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></oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">1000</oasis:entry>  
         <oasis:entry colname="col2">150 ns</oasis:entry>  
         <oasis:entry colname="col3">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></oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1">5000</oasis:entry>  
         <oasis:entry colname="col2">100 ns</oasis:entry>  
         <oasis:entry colname="col3">2.5 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></oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup><?xmltex \end{scaleboxenv}?></oasis:table></table-wrap>

      <?xmltex \floatpos{t}?><fig id="Ch1.F5"><caption><p>Principle drawing for the combined measurement of thickness and
sound velocity by means of a focusing transducer.</p></caption>
        <?xmltex \igopts{width=241.848425pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f05.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F6" specific-use="star"><caption><p>Left: focusing curves for different control sound velocities;
right: determination of sound velocity by intersection of two curves; Red
curve: reflector distance as a function of sound velocity and measured ToF.
Blue curve: reflector distance as a function of the control sound velocity
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mi mathvariant="normal">control</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>; Blue points: four pairs of sound velocity and corresponding
distance are determined by focusing curves.</p></caption>
        <?xmltex \igopts{width=384.112205pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f06.png"/>

      </fig>

      <p>The current work deals with generating calibration curves for media with
continuously changing properties. The continuous change of material
properties is taken into account by a modified wave equation. The potential
of a point source has been calculated in the Hankel transformed domain. The
inverse transform is realized and allows calculating Green's functions for media with continuously changing properties for a change of
material properties in axial direction of the array (Wolf and Kühnicke,  2015). A
change of these properties in other directions would cause a lateral
deviation of the focus position and has to be examined in further works.
Further advances of the method are planned for measuring sound velocity
profiles in media with stationary particles (e.g. medical tissues).</p>
</sec>
<sec id="Ch1.S3">
  <title>Simultaneous determination of thickness and sound velocity</title>
      <p>For imaging in NDT or in medical diagnostics, the value of sound velocity is
assumed a priori. Interfaces of hidden objects (defects, surfaces of organs,
vessels) are imaged by the measured ToF. The supposed
locations and the extensions of objects are incorrect if the real speed of
sound differs from the assumption.</p>
      <p>For material characterization the thickness of a specimen is measured (e.g.
mechanically) and the sound velocity is determined by ToF measurements. If
there is a multi-layered structure, the mechanical determination of the
thickness of the different layers can impossibly be done non-destructively.
It is necessary to determine both quantities simultaneously to get
information about the thicknesses and the materials of the different layers.</p>
      <p>To satisfy the demands of NDT, novel approaches evaluate the sound field,
which depends on the propagation medium. Gust (2011) determines sound
velocity and thickness of plates with a scanning acoustic microscope by
moving a probe in water vertically to the surface. The focus position is
used as a second measuring quantity in addition to the propagation time. The
echo of the surface and of the back wall is maximal if the focus is located
on it (compare signals for position 2 and 3, Fig. 5). The displacement
between the transducer positions, where the echo of the first and the second
interface become strongest, is determined. Because the focus position
depends on the sound velocity, the necessary displacement differs dependent on the material of the plates, even for plates of the same
thickness. So the displacement and the ToF between the interfaces
can be used to determine sound velocity and thickness simultaneously.</p><?xmltex \hack{\newpage}?><?xmltex \floatpos{t}?><fig id="Ch1.F7" specific-use="star"><caption><p>Signals for different propagation paths.</p></caption>
        <?xmltex \igopts{width=384.112205pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f07.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F8"><caption><p>The time of flight of the ultrasonic wave between the inner and
outer transducer elements (numbers 1–5) of an annular array depends on the
reflector curvature. The larger the sphere, the shorter the propagation
path is from the innermost element to the outer elements.</p></caption>
        <?xmltex \igopts{width=170.716535pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f08.png"/>

      </fig>

      <?xmltex \floatpos{t}?><fig id="Ch1.F9" specific-use="star"><caption><p>Measured echo signals for the propagation paths (S1/R1) and
(S1/R4) of a plane annular array with five elements for sphere radii of 6
and 10 mm (S: sending element, R: receiving element). The sphere is located
at <inline-formula><mml:math display="inline"><mml:mi>z</mml:mi></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> 13 mm, which is the near-field length of the single elements of the
annular array.</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f09.png"/>

      </fig>

      <p>A method is introduced by Kümmritz et al. (2015) allowing a simultaneous
determination of sound velocity and thickness of up to two layers with an
annular array at a fixed position. It works by varying the control mode to
move the focus position along the acoustic axis. The amplitudes of the echo
signals are evaluated to get additional information beside the ToF. A measurement set-up with a water delay line between the specimen
and a plane annular array with a centre frequency of 6 MHz is used.</p>
      <p>The approach is explained by analysing a first liquid layer. The focus
position is continuously moved along the acoustic axis by changing the
control mode calculated on the basis of different assumed control sound
velocities <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mi mathvariant="normal">control</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula>. In contrast to the approach with scatterers the
control sound velocity is varied. In Fig. 6 (right curve), a control sound
velocity of 1000 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> is used to calculate the delay times. The back wall
echo signal is determined, and its amplitude is recorded as a function of
the control mode. The result is the blue focusing curve on the right side.
At 30 mm, a maximum can be seen. This maximum indicates that if the sound
velocity of the fluid was 1000 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>, the thickness of the first layer would
be 30 mm. The process is repeated for different control velocities
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mi mathvariant="normal">control</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> (Fig. 6, left), and the supposed thickness is recorded as a
function of control sound velocity (Fig. 6, right blue line).</p>
      <p>The ToF between probe and surface gives additional information (red line).
The correct sound velocity and thickness of the specimen is the intersection
of the two curves.</p>
      <p>After the determination of thickness and velocity of the first layer, the
approach is repeated for the second layer. Refraction effects have to be
taken into account to correctly focus into the second medium. The delay
times are determined by means of Fermat's principle. The thickness and sound
velocity of the first layer have to be known for this.</p>
      <p>Measurements were done for a two-layered structure with the first layer of
water and the second layer of steel or aluminum with a thickness
<inline-formula><mml:math display="inline"><mml:mrow><mml:mi>d</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">6</mml:mn></mml:mrow></mml:math></inline-formula>, 8, 10, 12 and 14 mm (Kümmritz et al., 2015). The
relative error was less than 1 %. For the second layer, a relative error
of less than 3 % had been achieved for the current measurement set-up.</p>
      <p>With this approach the delay times, where the focused echo signal becomes
maximal, are iteratively determined, which means that they interfere
maximally
positively. Figure 9 exemplarily shows the signals transceiving with the
central element and the third ring. Whereas there is only one signal for the
central element, two signal parts can be recognized for the third ring. The
two signal parts can be related geometrically to two different propagation
paths: the direct wave with normal incidence and the wave which is received
at the opposite site of the ring (see Fig. 7, left). The second signal part
of the third ring has to interfere with the single signal of the central
element for optimal focusing. This means that the “correct” delay times
can be determined directly from the signal without focusing, which leads to
another approach determining thickness and sound velocity with these delay
times and an inverse model.</p>
      <p>As a first step the signal parts have to be separated as they interfere for
the inner elements. The signal of the central element is chosen as reference
signal because it has a propagation path with normal incidence. Due to small
phase shifts in the signal first the analytic signal <inline-formula><mml:math display="inline"><mml:mrow><mml:msubsup><mml:mi>s</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mi mathvariant="normal">H</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> is
calculated by Hilbert transform of signal <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> emitted by element <inline-formula><mml:math display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula> and
received by element <inline-formula><mml:math display="inline"><mml:mi>j</mml:mi></mml:math></inline-formula>.</p>
      <p>The mean phase difference is calculated and used to shift the reference
signal. Finally the real part of the difference of analysed and phase
shifted reference signal is calculated. This yields a difference signal
<inline-formula><mml:math display="inline"><mml:mrow><mml:msup><mml:mi>s</mml:mi><mml:mi mathvariant="normal">D</mml:mi></mml:msup></mml:mrow></mml:math></inline-formula> containing only the second signal part.

              <disp-formula id="Ch1.E1" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msubsup><mml:mi>s</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">D</mml:mi></mml:msubsup><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mi mathvariant="normal">ℜ</mml:mi><mml:mfenced close="]" open="["><mml:msubsup><mml:mi>s</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mi mathvariant="normal">H</mml:mi></mml:msubsup><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>-</mml:mo><mml:msubsup><mml:mi>s</mml:mi><mml:mn>11</mml:mn><mml:mi mathvariant="normal">H</mml:mi></mml:msubsup><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:msup><mml:mi>e</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mo>(</mml:mo><mml:mo>(</mml:mo><mml:msubsup><mml:mi>s</mml:mi><mml:mrow><mml:mi>j</mml:mi><mml:mi>i</mml:mi></mml:mrow><mml:mi mathvariant="normal">H</mml:mi></mml:msubsup><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>)</mml:mo><mml:mo>-</mml:mo><mml:mo>(</mml:mo><mml:msubsup><mml:mi>s</mml:mi><mml:mn>11</mml:mn><mml:mi mathvariant="normal">H</mml:mi></mml:msubsup><mml:mo>(</mml:mo><mml:mi>t</mml:mi><mml:mo>)</mml:mo><mml:mo>)</mml:mo><mml:mo>)</mml:mo></mml:mrow></mml:msup></mml:mfenced></mml:mrow></mml:math></disp-formula></p>
      <p>The “correct” delay time is now determined by cross-correlating
<inline-formula><mml:math display="inline"><mml:mrow><mml:msubsup><mml:mi>s</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow><mml:mi mathvariant="normal">D</mml:mi></mml:msubsup></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>s</mml:mi><mml:mn>11</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>.</p>
      <p>Additionally a geometric model is applied. It calculates the ToF
as a function of thickness and sound velocity of the second layer.

              <disp-formula id="Ch1.E2" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi>t</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">E</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">D</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>-</mml:mo><mml:msubsup><mml:mi>z</mml:mi><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:msqrt><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>+</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:mo>(</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">D</mml:mi></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">R</mml:mi></mml:msub><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:msubsup><mml:mi>z</mml:mi><mml:mn mathvariant="normal">2</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:msqrt><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>

        with

              <disp-formula id="Ch1.E3" content-type="numbered"><mml:math display="block"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">E</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>r</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>,</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">R</mml:mi></mml:msub><mml:mo>=</mml:mo><mml:mo>(</mml:mo><mml:msub><mml:mi>r</mml:mi><mml:mi>i</mml:mi></mml:msub><mml:mo>+</mml:mo><mml:msub><mml:mi>r</mml:mi><mml:mi>j</mml:mi></mml:msub><mml:mo>)</mml:mo><mml:mo>/</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mo>,</mml:mo></mml:mrow></mml:math></disp-formula>

        where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mi>i</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>r</mml:mi><mml:mi>j</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> are the mean radii of emitter <inline-formula><mml:math display="inline"><mml:mi>i</mml:mi></mml:math></inline-formula> and receiver <inline-formula><mml:math display="inline"><mml:mi>j</mml:mi></mml:math></inline-formula>, <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</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>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> the (known) thickness and sound velocity of the first medium,
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> and <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> the (unknown) thickness and sound velocity of the
investigated layer. Also the coordinate <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">D</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> of the point <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>P</mml:mi><mml:mi mathvariant="normal">D</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> is
unknown, but it can be determined by Fermat's principle, meaning that the
ToF must be minimal. Taking into account that <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> is connected
with <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> by the ToF <inline-formula><mml:math display="inline"><mml:mi>T</mml:mi></mml:math></inline-formula> between surface and back wall echoes it
can be replaced with <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>z</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>=</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:msub><mml:mi>T</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>/</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:mrow></mml:math></inline-formula>. This leads to

              <disp-formula specific-use="align" content-type="numbered"><mml:math display="block"><mml:mtable displaystyle="true"><mml:mtr><mml:mtd/><mml:mtd><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>=</mml:mo><mml:mi>f</mml:mi><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>)</mml:mo><mml:mo>=</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:mo>[</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi>E</mml:mi><mml:mo>,</mml:mo><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>-</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">D</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>)</mml:mo><mml:msup><mml:mo>]</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>-</mml:mo><mml:msubsup><mml:mi>z</mml:mi><mml:mn mathvariant="normal">1</mml:mn><mml:mn mathvariant="normal">2</mml:mn></mml:msubsup></mml:mrow></mml:msqrt><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">1</mml:mn></mml:msub></mml:mrow></mml:mfrac></mml:mstyle></mml:mrow></mml:mtd></mml:mtr><mml:mlabeledtr id="Ch1.E4"><mml:mtd/><mml:mtd/><mml:mtd><mml:mrow><?xmltex \hack{\hspace{0.8cm}}?><mml:mo>+</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:mstyle displaystyle="true"><mml:mfrac style="display"><mml:msqrt><mml:mrow><mml:mo>[</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">D</mml:mi></mml:msub><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>)</mml:mo><mml:mo>-</mml:mo><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">R</mml:mi><mml:mo>,</mml:mo><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:msup><mml:mo>]</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>+</mml:mo><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mi>T</mml:mi><mml:mo>/</mml:mo><mml:mn mathvariant="normal">2</mml:mn><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup></mml:mrow></mml:msqrt><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:mfrac></mml:mstyle><mml:mo>,</mml:mo></mml:mrow></mml:mtd></mml:mlabeledtr></mml:mtable></mml:math></disp-formula>

          where <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> is a function of the (solely unknown) variable <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>.
Combining the measured time differences <inline-formula><mml:math display="inline"><mml:mrow><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> with these
functions allows the determination of <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula> with the least-squares method.

              <disp-formula id="Ch1.E5" content-type="numbered"><mml:math display="block"><mml:mrow><mml:mi>F</mml:mi><mml:mo>=</mml:mo><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>i</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>N</mml:mi></mml:munderover><mml:munderover><mml:mo movablelimits="false">∑</mml:mo><mml:mrow><mml:mi>j</mml:mi><mml:mo>=</mml:mo><mml:mn mathvariant="normal">1</mml:mn></mml:mrow><mml:mi>N</mml:mi></mml:munderover><mml:mo>(</mml:mo><mml:mi mathvariant="normal">Δ</mml:mi><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>-</mml:mo><mml:mo>(</mml:mo><mml:msub><mml:mi>t</mml:mi><mml:mrow><mml:mi>i</mml:mi><mml:mi>j</mml:mi></mml:mrow></mml:msub><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>)</mml:mo><mml:mo>-</mml:mo><mml:msub><mml:mi>t</mml:mi><mml:mn>11</mml:mn></mml:msub><mml:mo>(</mml:mo><mml:msub><mml:mi>c</mml:mi><mml:mn mathvariant="normal">2</mml:mn></mml:msub><mml:mo>)</mml:mo><mml:mo>)</mml:mo><mml:msup><mml:mo>)</mml:mo><mml:mn mathvariant="normal">2</mml:mn></mml:msup><mml:mo>→</mml:mo><mml:mo movablelimits="false">min⁡</mml:mo></mml:mrow></mml:math></disp-formula>

        Of course, the determined sound velocity provides the thickness of the
layer.</p>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T2"><caption><p>Comparison of time differences between the two echo parts gained
from sound field simulation (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">sim</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> and determined with a geometric
model via Fermat's principle (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">geo</mml:mi></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula>.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="6">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="right"/>
     <oasis:colspec colnum="3" colname="col3" align="right"/>
     <oasis:colspec colnum="4" colname="col4" align="right"/>
     <oasis:colspec colnum="5" colname="col5" align="right"/>
     <oasis:colspec colnum="6" colname="col6" align="right"/>
     <oasis:thead>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1"/>  
         <oasis:entry colname="col2"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mn>22</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>[ns]</oasis:entry>  
         <oasis:entry colname="col3"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mn>33</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>[ns]</oasis:entry>  
         <oasis:entry colname="col4"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mn>44</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>[ns]</oasis:entry>  
         <oasis:entry colname="col5"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mn>55</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>[ns]</oasis:entry>  
         <oasis:entry colname="col6"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mn>66</mml:mn></mml:msub></mml:mrow></mml:math></inline-formula>[ns]</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">sim</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col2">160</oasis:entry>  
         <oasis:entry colname="col3">212</oasis:entry>  
         <oasis:entry colname="col4">276</oasis:entry>  
         <oasis:entry colname="col5">396</oasis:entry>  
         <oasis:entry colname="col6">540</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>t</mml:mi><mml:mi mathvariant="normal">geo</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula></oasis:entry>  
         <oasis:entry colname="col2">97</oasis:entry>  
         <oasis:entry colname="col3">197</oasis:entry>  
         <oasis:entry colname="col4">299</oasis:entry>  
         <oasis:entry colname="col5">405</oasis:entry>  
         <oasis:entry colname="col6">548</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

<?xmltex \floatpos{t}?><table-wrap id="Ch1.T3"><caption><p>Different attaching points for geometric model used in Eq. (4):
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">geo</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> gained from main radii of array electrodes; <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">corr</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> adapted
points so that time differences (see Table 3) from geometric model and from
sound field simulations agree.</p></caption><oasis:table frame="topbot"><?xmltex \begin{scaleboxenv}{.98}[.98]?><oasis:tgroup cols="7">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="right"/>
     <oasis:colspec colnum="3" colname="col3" align="right"/>
     <oasis:colspec colnum="4" colname="col4" align="right"/>
     <oasis:colspec colnum="5" colname="col5" align="right"/>
     <oasis:colspec colnum="6" colname="col6" align="right"/>
     <oasis:colspec colnum="7" colname="col7" align="right"/>
     <oasis:thead>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1">Element</oasis:entry>  
         <oasis:entry colname="col2">1</oasis:entry>  
         <oasis:entry colname="col3">2</oasis:entry>  
         <oasis:entry colname="col4">3</oasis:entry>  
         <oasis:entry colname="col5">4</oasis:entry>  
         <oasis:entry colname="col6">5</oasis:entry>  
         <oasis:entry colname="col7">6</oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">geo</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> [mm]</oasis:entry>  
         <oasis:entry colname="col2">1.58</oasis:entry>  
         <oasis:entry colname="col3">2.90</oasis:entry>  
         <oasis:entry colname="col4">3.85</oasis:entry>  
         <oasis:entry colname="col5">4.64</oasis:entry>  
         <oasis:entry colname="col6">5.34</oasis:entry>  
         <oasis:entry colname="col7">6.19</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">corr</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> [mm]</oasis:entry>  
         <oasis:entry colname="col2">1.58</oasis:entry>  
         <oasis:entry colname="col3">3.24</oasis:entry>  
         <oasis:entry colname="col4">3.55</oasis:entry>  
         <oasis:entry colname="col5">4.76</oasis:entry>  
         <oasis:entry colname="col6">5.47</oasis:entry>  
         <oasis:entry colname="col7">6.39</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup><?xmltex \end{scaleboxenv}?></oasis:table></table-wrap>

      <p>As this geometric model neglects the wave behaviour of the sound, additional
sound field simulations are done. The reflected signal is calculated by a
harmonic synthesis convolving the excitation signal with the frequency
components of the sound field. As the thickness and sound velocity are
defined in simulation these calculated signals can be used to compare the
resulting time differences with them from the geometric model. An example is
shown in Table 2.</p><?xmltex \hack{\newpage}?><?xmltex \floatpos{t}?><table-wrap id="Ch1.T4" specific-use="star"><caption><p>Comparison of determined sound velocities with the attaching points
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">geo</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> (from array geometry) and corrected <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">corr</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> via sound
field simulations.</p></caption><oasis:table frame="topbot"><oasis:tgroup cols="11">
     <oasis:colspec colnum="1" colname="col1" align="left"/>
     <oasis:colspec colnum="2" colname="col2" align="right"/>
     <oasis:colspec colnum="3" colname="col3" align="right"/>
     <oasis:colspec colnum="4" colname="col4" align="right"/>
     <oasis:colspec colnum="5" colname="col5" align="right"/>
     <oasis:colspec colnum="6" colname="col6" align="right" colsep="1"/>
     <oasis:colspec colnum="7" colname="col7" align="right"/>
     <oasis:colspec colnum="8" colname="col8" align="right"/>
     <oasis:colspec colnum="9" colname="col9" align="right"/>
     <oasis:colspec colnum="10" colname="col10" align="right"/>
     <oasis:colspec colnum="11" colname="col11" align="right"/>
     <oasis:thead>
       <oasis:row rowsep="1">  
         <oasis:entry colname="col1">Delay line</oasis:entry>  
         <oasis:entry namest="col2" nameend="col6" align="center">15 mm </oasis:entry>  
         <oasis:entry namest="col7" nameend="col11" align="center">20 mm </oasis:entry>
       </oasis:row>
     </oasis:thead>
     <oasis:tbody>
       <oasis:row>  
         <oasis:entry colname="col1"><inline-formula><mml:math display="inline"><mml:mrow><mml:mi>t</mml:mi><mml:mspace linebreak="nobreak" width="0.25em"/><mml:mi>d</mml:mi></mml:mrow></mml:math></inline-formula> [mm]</oasis:entry>  
         <oasis:entry colname="col2">4</oasis:entry>  
         <oasis:entry colname="col3">6</oasis:entry>  
         <oasis:entry colname="col4">8</oasis:entry>  
         <oasis:entry colname="col5">10</oasis:entry>  
         <oasis:entry colname="col6">14</oasis:entry>  
         <oasis:entry colname="col7">4 mm</oasis:entry>  
         <oasis:entry colname="col8">6 mm</oasis:entry>  
         <oasis:entry colname="col9">8 mm</oasis:entry>  
         <oasis:entry colname="col10">10</oasis:entry>  
         <oasis:entry colname="col11">14</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mi mathvariant="normal">geo</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> [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>]</oasis:entry>  
         <oasis:entry colname="col2">5688</oasis:entry>  
         <oasis:entry colname="col3">5787</oasis:entry>  
         <oasis:entry colname="col4">–</oasis:entry>  
         <oasis:entry colname="col5">–</oasis:entry>  
         <oasis:entry colname="col6">5649</oasis:entry>  
         <oasis:entry colname="col7">5682</oasis:entry>  
         <oasis:entry colname="col8">5765</oasis:entry>  
         <oasis:entry colname="col9">5647</oasis:entry>  
         <oasis:entry colname="col10">5772</oasis:entry>  
         <oasis:entry colname="col11">5688</oasis:entry>
       </oasis:row>
       <oasis:row>  
         <oasis:entry colname="col1"><inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>c</mml:mi><mml:mi mathvariant="normal">corr</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> [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>]</oasis:entry>  
         <oasis:entry colname="col2">5866</oasis:entry>  
         <oasis:entry colname="col3">5920</oasis:entry>  
         <oasis:entry colname="col4">5923</oasis:entry>  
         <oasis:entry colname="col5">5960</oasis:entry>  
         <oasis:entry colname="col6">5929</oasis:entry>  
         <oasis:entry colname="col7">5883</oasis:entry>  
         <oasis:entry colname="col8">5902</oasis:entry>  
         <oasis:entry colname="col9">5909</oasis:entry>  
         <oasis:entry colname="col10">5939</oasis:entry>  
         <oasis:entry colname="col11">5866</oasis:entry>
       </oasis:row>
     </oasis:tbody>
   </oasis:tgroup></oasis:table></table-wrap>

      <?xmltex \floatpos{t}?><fig id="Ch1.F10" specific-use="star"><caption><p>Focused sound emission with two opposite 90<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> transducer
segments each being divided in radial direction into four elements (left
figure). The focusing curves allow the determination of the half-axes of the
reflector (right figure).</p></caption>
        <?xmltex \igopts{width=341.433071pt}?><graphic xlink:href="https://jsss.copernicus.org/articles/5/373/2016/jsss-5-373-2016-f10.png"/>

      </fig>

      <p>As expected the times differ significantly because the geometric model would
only be valid for plane waves. The coordinate <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mi mathvariant="normal">E</mml:mi></mml:msub></mml:mrow></mml:math></inline-formula> in the geometric model
had been chosen as the mean radius of the element (<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">geo</mml:mi></mml:mrow></mml:msub><mml:mo>)</mml:mo></mml:mrow></mml:math></inline-formula> but can be
chosen arbitrarily. So the sound field simulations can be used to modify the
model parameters: <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">corr</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> is determined so that the geometric model
gives the times gained from simulation. Table 3 compares the mean radii
<inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">geo</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> with the corrected ones <inline-formula><mml:math display="inline"><mml:mrow><mml:msub><mml:mi>y</mml:mi><mml:mrow><mml:mi mathvariant="normal">E</mml:mi><mml:mo>,</mml:mo><mml:mi mathvariant="normal">corr</mml:mi></mml:mrow></mml:msub></mml:mrow></mml:math></inline-formula> and Table 4 the
sound velocities determined with both.</p>
</sec>
<sec id="Ch1.S4">
  <title>Curvature measurements</title>
      <p>When measuring in pulse-echo mode, the reflected ultrasonic wave contains not
only information about material parameters such as the sound
velocities in a layered structure but also some information about the local
inclination angle toward the acoustic axis and the curvature of the
reflector.</p>
      <p>While the information about the reflector inclination is mainly contained in
the angle of reflection of the reflected wave, the information about the
reflector curvature is contained in the wave front curvature and the arrival
times of the reflected wave on the different elements of an annular array.</p>
      <p>In Fig. 8 it can be seen that the propagation path lengths between the inner
element of an annular array and the outer elements show a dependence on the
reflector radius.</p>
      <p>In Fig. 9 measurements were done to distinguish reflectors and determine the
reflector curvature of spheres being kept in a water bath. While the ToF of the wave propagating along the acoustic axis is the same for both
reflector radii (Fig. 9, left), the ToF from the innermost
element to the outer element with number four depends on the reflector
radius (Fig. 9, right). Under the given conditions, sphere radii could be
determined with an uncertainty of about 0.5 mm, where spheres of between
6 and 11 mm radius were used in the experiments (Lenz, 2013).</p>
      <p>A further segmentation of the annular array in four 90<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> pieces
enables the differentiation of the half-axes of a rotational ellipsoid. In
the following measurements, the 90<inline-formula><mml:math display="inline"><mml:msup><mml:mi/><mml:mo>∘</mml:mo></mml:msup></mml:math></inline-formula> segments on the opposite
sides of the transducer were always used together, where the half-axes of
the reflector were put parallel to the symmetry axes of the transducer
(Fig. 10, left).</p>
      <p>Instead of measuring time delays of different propagation paths, as in the
set-up of Fig. 9, the transducer was focused here and the echo signal
amplitude was plotted as a function of the focus setting <italic>Fok</italic>, i. e. the set of
delay times focusing at a distance of <inline-formula><mml:math display="inline"><mml:mi>z</mml:mi></mml:math></inline-formula> <inline-formula><mml:math display="inline"><mml:mo>=</mml:mo></mml:math></inline-formula> <italic>Fok</italic> on the acoustic axis. As can be
seen in Fig. 10 (right), the different half-axes of an elliptical reflector
can be distinguished by comparing the maximum positions of the focusing
curves.</p>
      <p>While the main drawback of the presented non-scanning curvature measurement
methods is the necessity for large transducer apertures and the high
cross-sensitivity of the method towards local inaccuracies of the surface,
the methods might be useful in the future to achieve additional pieces of
information in scanning and non-scanning applications in NDT and medical
engineering.</p><?xmltex \hack{\newpage}?>
</sec>
<sec id="Ch1.S5">
  <title>Data availability</title>
      <p>The data are not available online. Please contact the authors to obtain access.</p>
</sec>
<sec id="Ch1.S6" sec-type="conclusions">
  <title>Summary</title>
      <p>Three approaches have been introduced which use the wave properties of
ultrasound instead of measuring simply the ToF. They allow the measurement of the
sound velocity in fluids and solids with one transducer and without the need
of additional reflectors at known positions. Whereas the scattering particle
method shall be applied for process monitoring and medical diagnostics the
method for measuring curvature, thickness and sound velocity shall be
applied in NDT and for material characterization. The development of all
methods required sound field simulations to predict the pressure
distribution on the transducer and to find evaluation criteria.</p>
</sec>

      
      </body>
    <back><ack><title>Acknowledgements</title><p>The authors would like to thank Deutsche Forschungsgemeinschaft (DFG) for
their financial support of the ongoing research project KU1075/17-1.<?xmltex \hack{\newline}?><?xmltex \hack{\newline}?>
Edited by:  O. Kanoun<?xmltex \hack{\newline}?>
Reviewed by:  three anonymous referees</p></ack><?xmltex \hack{\newpage}?><?xmltex \hack{\newpage}?><ref-list>
    <title>References</title>

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USA, 18–21 October 2011.
 </mixed-citation></ref><?xmltex \hack{\newpage}?>
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Kümmritz, S., Wolf, M., and Kühnicke, E.: Simultane Bestimmung von
Dicken und Schallgeschwindigkeiten geschichteter Strukturen, tm – Technisches
Messen 82/3, 127–134, 2015.</mixed-citation></ref>
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Wolf, M., Kühnicke, E., and  Lenz, M.: Modeling of sound propagation in
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measurement of sound velocity, IEEE International Ultrasonics Symposium
(IUS), 1045–1048,  Prague, Czech Republic, 21–25 July 2013.</mixed-citation></ref>
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  </ref-list><app-group content-type="float"><app><title/>

    </app></app-group></back>
    <!--<article-title-html>Annular arrays for novel ultrasonic  measurement techniques</article-title-html>
<abstract-html><p class="p">The paper shows how the precise knowledge of the sound field of an
ultrasonic annular array can contribute to the development of novel
measurement techniques. Emphasis is placed on (a) a non-invasive method for
sound velocity measurements in fluids using the echo signals from scattering
p]articles, (b) a non-invasive method for the combined determination of
thickness and sound velocity in layered structures by using a novel focusing
technique, and (c) a non-scanning curvature measurement method exploiting the
wave front curvature of a reflected wave. To demonstrate the methods, the
principles as well as results of simulations and measurements are discussed.</p></abstract-html>
<ref-html id="bib1.bib1"><label>1</label><mixed-citation>
Dayal, V.: An automated simultaneous measurement of thickness and wave
velocity by ultrasound, Experimental mechanics,   197–202, September 1992.
</mixed-citation></ref-html>
<ref-html id="bib1.bib2"><label>2</label><mixed-citation>
Gust, N.: Improvement of signal analysis for ultrasonic microscopy,
Dissertation Technische Universität Dresden, ISBN-13: 978-3-942710-22-0,
2011.
</mixed-citation></ref-html>
<ref-html id="bib1.bib3"><label>3</label><mixed-citation>
Huang, S.-H. and Li, P.-C.: Computed Tomography Sound Velocity
Reconstruction Using Incomplete Data,  IEEE T. Ultrason.
Ferr., 51, 329–342, 2004.
</mixed-citation></ref-html>
<ref-html id="bib1.bib4"><label>4</label><mixed-citation>
Hsu, D. K. and Hughes, M. S.: Simultaneous ultrasonic velocity and sample
thickness measurement and application in composites,  J. Acoust. Soc. Am., 92, 669–675, 1992.
</mixed-citation></ref-html>
<ref-html id="bib1.bib5"><label>5</label><mixed-citation>
Janas, V. and Safari, A.: Overview of Fine-Scale Piezoelectric Ceramic/Polymer
Composite Processing, J. Am. Ceram. Soc., 78, 2945–2955,
<a href="http://dx.doi.org/10.1111/j.1151-2916.1995.tb09068.x" target="_blank">doi:10.1111/j.1151-2916.1995.tb09068.x</a>, 1995.
</mixed-citation></ref-html>
<ref-html id="bib1.bib6"><label>6</label><mixed-citation>
Kim, Y. H., Song, S., and Lee, J.: Simultaneous measurements of the
ultrasonic wave velocity and thickness of a solid plate made from one side of
the plate, Measurement Science and Technology, 14, p. N13, 2003.
</mixed-citation></ref-html>
<ref-html id="bib1.bib7"><label>7</label><mixed-citation>
Kühnicke, E.: Plane arrays – Fundamental investigations for correct
steering by means of sound field calculations, Wave Motion, 44, 248–261,
<a href="http://dx.doi.org/10.1016/j.wavemoti.2006.10.003" target="_blank">doi:10.1016/j.wavemoti.2006.10.003</a>, 2007.
</mixed-citation></ref-html>
<ref-html id="bib1.bib8"><label>8</label><mixed-citation>
Kühnicke, E., Lenz, M., and Bock, M.: Non-invasive measurement of sound
velocity profiles, IEEE International Ultrasonics Symposium, 2151–2153, Orlando,
USA, 18–21 October 2011.

</mixed-citation></ref-html>
<ref-html id="bib1.bib9"><label>9</label><mixed-citation>
Kümmritz, S., Wolf, M., and Kühnicke, E.: Simultane Bestimmung von
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