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    <datestamp>2004-06-10</datestamp>
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    <creators>
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        <name>
          <family>Dellar</family>
          <given>P.</given>
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          <family>Howell</family>
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    <contributors>
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          <family>Dewynne</family>
          <given>J.</given>
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        <id></id>
      </item>
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        <type></type>
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          <family>Edwards</family>
          <given>C.M.</given>
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          <family>Ockendon</family>
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          <family>Ockendon</family>
          <given>J.R.</given>
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        <type></type>
        <name>
          <family>Please</family>
          <given>C.P.</given>
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        <type></type>
        <name>
          <family>Salazar-Gonzales</family>
          <given>D.</given>
        </name>
        <id></id>
      </item>
    </contributors>
    <title>Shock-free Supersonic Transport</title>
    <ispublished>pub</ispublished>
    <subjects>
      <item>aerodef</item>
    </subjects>
    <studygroups>esgi40</studygroups>
    <companyname>Vehicle Research Corporation</companyname>
    <full_text_status>public</full_text_status>
    <problem_statement>Vehicle Research Corporation has proposed a mechanism for eliminating the sonic boom generated by supersonic flight. It involves a nozzle-shaped wing underside, together with an underwing planar jet of engine compressor air. The Study Group was asked to provide a critical review of the proposed mechanism and a quantitative analysis of its likely performance.</problem_statement>
    <date>2001-04</date>
    <date_type>published</date_type>
    <pages>11</pages>
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        <main>ShockFree.pdf</main>
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