<?xml version="1.0" encoding="UTF-8"?>
<crossref_result xmlns="http://www.crossref.org/qrschema/3.0" version="3.0" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.crossref.org/qrschema/3.0 http://www.crossref.org/schemas/crossref_query_output3.0.xsd">
  <query_result>
    <head>
      <doi_batch_id>none</doi_batch_id>
    </head>
    <body>
      <query status="resolved">
        <doi type="journal_article">10.1260/1757-2258.4.1-2.13</doi>
        <crm-item name="publisher-name" type="string">Portico</crm-item>
        <crm-item name="prefix-name" type="string">Portico</crm-item>
        <crm-item name="member-id" type="number">1320</crm-item>
        <crm-item name="citation-id" type="number">58598915</crm-item>
        <crm-item name="journal-id" type="number">96649</crm-item>
        <crm-item name="deposit-timestamp" type="number">2015061210344500809</crm-item>
        <crm-item name="owner-prefix" type="string">10.3730</crm-item>
        <crm-item name="last-update" type="date">2017-10-04T12:48:54Z</crm-item>
        <crm-item name="created" type="date">2012-11-16T21:59:34Z</crm-item>
        <crm-item name="citedby-count" type="number">3</crm-item>
        <doi_record>
          <crossref xmlns="http://www.crossref.org/xschema/1.1" xsi:schemaLocation="http://www.crossref.org/xschema/1.1 http://doi.crossref.org/schemas/unixref1.1.xsd">
            <journal>
              <journal_metadata language="en">
                <full_title>International Journal of Aerospace Innovations</full_title>
                <abbrev_title>International Journal of Aerospace Innovations</abbrev_title>
                <issn media_type="print">1757-2258</issn>
              </journal_metadata>
              <journal_issue>
                <publication_date media_type="print">
                  <month>03</month>
                  <year>2012</year>
                </publication_date>
                <journal_volume>
                  <volume>4</volume>
                </journal_volume>
                <issue>1-2</issue>
              </journal_issue>
              <journal_article publication_type="full_text">
                <titles>
                  <title>Flow Topology and Secondary Separation Modelling at Crossing Shock Wave/Turbulent Boundary Layer Interaction Conditions</title>
                </titles>
                <contributors>
                  <person_name sequence="first" contributor_role="author">
                    <given_name>Andrea</given_name>
                    <surname>Salin</surname>
                  </person_name>
                  <person_name sequence="additional" contributor_role="author">
                    <given_name>Yufeng</given_name>
                    <surname>Yao</surname>
                  </person_name>
                  <person_name sequence="additional" contributor_role="author">
                    <given_name>Alexander</given_name>
                    <surname>Zheltovodov</surname>
                  </person_name>
                </contributors>
                <publication_date media_type="print">
                  <month>03</month>
                  <year>2012</year>
                </publication_date>
                <pages>
                  <first_page>13</first_page>
                  <last_page>28</last_page>
                </pages>
                <publisher_item>
                  <identifier id_type="doi">10.1260/1757-2258.4.1-2.13</identifier>
                </publisher_item>
                <doi_data>
                  <doi>10.1260/1757-2258.4.1-2.13</doi>
                  <resource>http://multi-science.atypon.com/doi/10.1260/1757-2258.4.1-2.13</resource>
                  <collection property="crawler-based">
                    <item crawler="google">
                      <resource>http://multi-science.metapress.com/index/JQ76JNG37464M50N.pdf</resource>
                    </item>
                  </collection>
                  <collection property="list-based" multi-resolution="unlock">
                    <item label="CLOCKSS_EDINA" setbyID="creftest">
                      <resource>http://triggered.edina.clockss.org/ServeContent?url=http%3A%2F%2Fmulti-science.atypon.com%2Fdoi%2Fpdf%2F10.1260%2F1757-2258.4.1-2.13</resource>
                    </item>
                    <item label="CLOCKSS_SU" setbyID="creftest">
                      <resource>http://triggered.stanford.clockss.org/ServeContent?url=http%3A%2F%2Fmulti-science.atypon.com%2Fdoi%2Fpdf%2F10.1260%2F1757-2258.4.1-2.13</resource>
                    </item>
                  </collection>
                </doi_data>
                <citation_list>
                  <citation key="1">
                    <journal_title>Progress in Aerospace Sciences</journal_title>
                    <author>D. Knight</author>
                    <volume>39</volume>
                    <issue>2-3</issue>
                    <first_page>121</first_page>
                    <cYear>2003</cYear>
                    <doi provider="crossref">10.1016/S0376-0421(02)00069-6</doi>
                    <article_title>Advances in CFD prediction of shock wave turbulent boundary layer interactions</article_title>
                  </citation>
                  <citation key="2">
                    <author>A. Zheltovodov</author>
                    <first_page>0496</first_page>
                    <cYear>2006</cYear>
                    <volume_title>Some advances in research of shock wave turbulent boundary layer interactions</volume_title>
                  </citation>
                  <citation key="3">
                    <author>A. Zheltovodov</author>
                    <first_page>202</first_page>
                    <cYear>2011</cYear>
                    <doi provider="crossref">10.1017/CBO9780511842757.005</doi>
                    <volume_title>Shock Wave-Boundary-Layer Interactions</volume_title>
                  </citation>
                  <citation key="4">
                    <journal_title>Aerospace Science and Technology</journal_title>
                    <author>F. Thivet</author>
                    <volume>6</volume>
                    <issue>1</issue>
                    <first_page>3</first_page>
                    <cYear>2002</cYear>
                    <doi provider="crossref">10.1016/S1270-9638(01)01133-6</doi>
                    <article_title>Analysis of observed and computed crossing-shock-wave/turbulent-boundary-layer interactions</article_title>
                  </citation>
                  <citation key="5">
                    <journal_title>AIAA Journal</journal_title>
                    <author>F. Thivet</author>
                    <volume>39</volume>
                    <issue>6</issue>
                    <first_page>985</first_page>
                    <cYear>2001</cYear>
                    <doi provider="crossref">10.2514/3.14831</doi>
                    <article_title>Insights in turbulence modelling for crossing-shock-wave/boundary-layer interactions</article_title>
                  </citation>
                  <citation key="6">
                    <journal_title>AIAA Journal</journal_title>
                    <author>D. Gaitonde</author>
                    <volume>33</volume>
                    <issue>12</issue>
                    <first_page>2250</first_page>
                    <cYear>1995</cYear>
                    <doi provider="crossref">10.2514/3.12976</doi>
                    <article_title>Structure of a turbulent double-fin interaction at Mach 4</article_title>
                  </citation>
                  <citation key="7">
                    <journal_title>J. Appl. Mech. Tech. Phys</journal_title>
                    <author>A. Zheltovodov</author>
                    <volume>23</volume>
                    <issue>3</issue>
                    <first_page>413</first_page>
                    <cYear>1982</cYear>
                    <doi provider="crossref">10.1007/BF00910085</doi>
                    <article_title>Regimes and properties of three-dimensional separation flow initiated by skewed compression shocks</article_title>
                  </citation>
                  <citation key="8">
                    <journal_title>J. Fluid Mech</journal_title>
                    <author>A. Panaras</author>
                    <volume>338</volume>
                    <first_page>203</first_page>
                    <cYear>1997</cYear>
                    <doi provider="crossref">10.1017/S0022112097004825</doi>
                    <article_title>The effect of the structure of swept-shock-wave/turbulent-boundary-layer interactions on turbulence modelling</article_title>
                  </citation>
                  <citation key="9">
                    <journal_title>Int. J. Heat &amp; Fluid Flow</journal_title>
                    <author>P. Durbin</author>
                    <volume>17</volume>
                    <issue>1</issue>
                    <first_page>89</first_page>
                    <cYear>1996</cYear>
                    <doi provider="crossref">10.1016/0142-727X(95)00073-Y</doi>
                    <article_title>On the k-ε stagnation point anomaly</article_title>
                  </citation>
                  <citation key="10">
                    <author>F. Thivet</author>
                    <cYear>2001</cYear>
                    <article_title>Importance of limiting the turbulence stresses to predict 3D shock wave boundary layer interactions</article_title>
                  </citation>
                  <citation key="11">
                    <journal_title>AIAA Journal</journal_title>
                    <author>A. Panaras</author>
                    <volume>35</volume>
                    <issue>3</issue>
                    <first_page>456</first_page>
                    <cYear>1997</cYear>
                    <doi provider="crossref">10.2514/3.13526</doi>
                    <article_title>Algebraic turbulence modelling for swept shock-wave/turbulent boundary-layer interactions</article_title>
                  </citation>
                  <citation key="12">
                    <journal_title>AIAA Journal</journal_title>
                    <author>T. Garrison</author>
                    <volume>32</volume>
                    <issue>7</issue>
                    <first_page>1234</first_page>
                    <cYear>1994</cYear>
                    <doi provider="crossref">10.2514/3.12125</doi>
                    <article_title>Laser Interferometer Skin-Friction Measurement of crossing-Shock-Wave/Turbulent-Boundary-Layer Interactions</article_title>
                  </citation>
                  <citation key="13">
                    <journal_title>AIAA Journal</journal_title>
                    <author>J. Schmisseur</author>
                    <volume>39</volume>
                    <issue>19</issue>
                    <first_page>1742</first_page>
                    <cYear>2001</cYear>
                    <doi provider="crossref">10.2514/2.1504</doi>
                    <article_title>Numerical investigation of new topologies in strong crossing shock-wave/turbulent boundary-layer interactions</article_title>
                  </citation>
                  <citation key="14">
                    <journal_title>AIAA Journal</journal_title>
                    <author>A. Panaras</author>
                    <volume>42</volume>
                    <issue>12</issue>
                    <first_page>2474</first_page>
                    <cYear>2004</cYear>
                    <doi provider="crossref">10.2514/1.12488</doi>
                    <article_title>Calculations of flows characterized by extensive crossflow separation</article_title>
                  </citation>
                  <citation key="15">
                    <author>E. Schülein</author>
                    <first_page>191</first_page>
                    <cYear>1998</cYear>
                    <article_title>Development of experimental methods for the hypersonic flows studies in Ludwieg tube</article_title>
                  </citation>
                  <citation key="16">
                    <journal_title>AIAA Paper</journal_title>
                    <author>F. Menter</author>
                    <first_page>2906</first_page>
                    <cYear>1993</cYear>
                    <article_title>Zonal Two Equation k-ε Turbulence Models for Aerodynamic Flows</article_title>
                  </citation>
                  <citation key="17">
                    <journal_title>AIAA Journal</journal_title>
                    <author>F. Menter</author>
                    <volume>32</volume>
                    <issue>8</issue>
                    <first_page>1598</first_page>
                    <cYear>1994</cYear>
                    <doi provider="crossref">10.2514/3.12149</doi>
                    <article_title>Two-Equation Eddy-Viscosity Turbulence Models for Engineering Applications</article_title>
                  </citation>
                  <citation key="18">
                    <journal_title>Thermophysics and Aeromechanics</journal_title>
                    <author>A. Zheltovodov</author>
                    <volume>5</volume>
                    <issue>3</issue>
                    <first_page>293</first_page>
                    <cYear>1998</cYear>
                    <article_title>Topology of three-dimensional separation under the conditions of symmetric interaction of crossing shocks and expansion waves with turbulent boundary layer</article_title>
                  </citation>
                  <citation key="19">
                    <journal_title>AIAA Paper</journal_title>
                    <author>Y. Yao</author>
                    <first_page>0860</first_page>
                    <cYear>2011</cYear>
                    <article_title>Numerical analysis of wall properties in cross shock wave and boundary layer interactions</article_title>
                  </citation>
                  <citation key="20">
                    <journal_title>Thermophysics and Aeromechanics</journal_title>
                    <author>A. Zheltovodov</author>
                    <volume>7</volume>
                    <issue>2</issue>
                    <first_page>155</first_page>
                    <cYear>2000</cYear>
                    <article_title>Experimental and numerical study of symmetric interaction of crossing-shocks and expansion-waves with a turbulent boundary layer</article_title>
                  </citation>
                  <citation key="21">
                    <author>A. Salin</author>
                    <cYear>2012</cYear>
                    <volume_title>Shock Waves</volume_title>
                  </citation>
                  <citation key="22">
                    <journal_title>Izvestiya AN SSSR, Mekhanika Zhidkosti i Gaza (Fluid Mechanics)</journal_title>
                    <author>A. Zheltovodov</author>
                    <volume>3</volume>
                    <first_page>42</first_page>
                    <cYear>1979</cYear>
                    <article_title>Physical features and properties of two- and three-dimensional separated flows at supersonic velocities</article_title>
                  </citation>
                  <citation key="23">
                    <author>A. Zheltovodov</author>
                    <first_page>67</first_page>
                    <cYear>1987</cYear>
                    <volume_title>Interaction of Complex 3-D Flows</volume_title>
                  </citation>
                  <citation key="24">
                    <journal_title>Izvestiya AN SSSR, Mekhanika Zhidkosti i Gaza (Fluid Mechanics)</journal_title>
                    <author>M. Zubin</author>
                    <volume>3</volume>
                    <first_page>51</first_page>
                    <cYear>1979</cYear>
                    <article_title>Structure of the flow in the region of separation for interaction of a normal shock wave with normal shock wave with a boundary layer</article_title>
                  </citation>
                </citation_list>
              </journal_article>
            </journal>
          </crossref>
        </doi_record>
      </query>
    </body>
  </query_result>
</crossref_result>