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Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests

Vos, Jan; Charbonnier, Dominique; Marwege, Ansgar; Guelhan Ali; Laureti, Mariasole; Karl, Sebastian


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  <identifier identifierType="URL">https://zenodo.org/record/5814915</identifier>
  <creators>
    <creator>
      <creatorName>Vos, Jan</creatorName>
      <givenName>Jan</givenName>
      <familyName>Vos</familyName>
      <nameIdentifier nameIdentifierScheme="ORCID" schemeURI="http://orcid.org/">0000-0003-1525-943X</nameIdentifier>
      <affiliation>CFS Engineering, EPFL Innovation Park - Bat. A, 1015 Lausanne, Switzerland</affiliation>
    </creator>
    <creator>
      <creatorName>Charbonnier, Dominique</creatorName>
      <givenName>Dominique</givenName>
      <familyName>Charbonnier</familyName>
      <nameIdentifier nameIdentifierScheme="ORCID" schemeURI="http://orcid.org/">0000-0002-9600-9258</nameIdentifier>
      <affiliation>Destinus SA,  Payerne, Switzerland,</affiliation>
    </creator>
    <creator>
      <creatorName>Marwege, Ansgar</creatorName>
      <givenName>Ansgar</givenName>
      <familyName>Marwege</familyName>
      <nameIdentifier nameIdentifierScheme="ORCID" schemeURI="http://orcid.org/">0000-0002-3912-9114</nameIdentifier>
      <affiliation>DLR Institute of Aerodynamics and Flow Technology, Supersonic and Hypersonic Technologies, 51147 Cologne, Germany</affiliation>
    </creator>
    <creator>
      <creatorName>Guelhan Ali</creatorName>
      <nameIdentifier nameIdentifierScheme="ORCID" schemeURI="http://orcid.org/">0000-0003-4905-5881</nameIdentifier>
      <affiliation>DLR Institute of Aerodynamics and Flow Technology, Supersonic and Hypersonic Technologies, 51147 Cologne, Germany</affiliation>
    </creator>
    <creator>
      <creatorName>Laureti, Mariasole</creatorName>
      <givenName>Mariasole</givenName>
      <familyName>Laureti</familyName>
      <nameIdentifier nameIdentifierScheme="ORCID" schemeURI="http://orcid.org/">0000-0001-5887-004X</nameIdentifier>
      <affiliation>DLR Institute of Aerodynamics and Flow Technology,  37073 Göttingen, Germany</affiliation>
    </creator>
    <creator>
      <creatorName>Karl, Sebastian</creatorName>
      <givenName>Sebastian</givenName>
      <familyName>Karl</familyName>
      <affiliation>DLR Institute of Aerodynamics and Flow Technology,  37073 Göttingen, Germany</affiliation>
    </creator>
  </creators>
  <titles>
    <title>Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests</title>
  </titles>
  <publisher>Zenodo</publisher>
  <publicationYear>2022</publicationYear>
  <dates>
    <date dateType="Issued">2022-01-05</date>
  </dates>
  <resourceType resourceTypeGeneral="ConferencePaper"/>
  <alternateIdentifiers>
    <alternateIdentifier alternateIdentifierType="url">https://zenodo.org/record/5814915</alternateIdentifier>
  </alternateIdentifiers>
  <relatedIdentifiers>
    <relatedIdentifier relatedIdentifierType="DOI" relationType="IsIdenticalTo">10.2514/6.2022-1308</relatedIdentifier>
    <relatedIdentifier relatedIdentifierType="URL" relationType="IsPartOf">https://zenodo.org/communities/retalt</relatedIdentifier>
  </relatedIdentifiers>
  <rightsList>
    <rights rightsURI="https://creativecommons.org/licenses/by/4.0/legalcode">Creative Commons Attribution 4.0 International</rights>
    <rights rightsURI="info:eu-repo/semantics/openAccess">Open Access</rights>
  </rightsList>
  <descriptions>
    <description descriptionType="Abstract">&lt;p&gt;In the RETALT (Retro Propulsion Assisted Landing Technologies) project critical technologies for two different vertical landing launcher configurations are investigated. For RETALT1, a Two Stage To Orbit launcher, only the first stage will be recovered using retro propulsion. A large number of wind tunnel experiments have been carried out at DLR in Cologne, while CFD simulations were made by CFS Engineering and DLR in G&amp;ouml;ttingen. This paper provides a detailed comparison of Wind Tunnel Experiments with CFD calculations in the hypersonic regime, with and without retro propulsion.&lt;/p&gt;</description>
  </descriptions>
  <fundingReferences>
    <fundingReference>
      <funderName>European Commission</funderName>
      <funderIdentifier funderIdentifierType="Crossref Funder ID">10.13039/100010661</funderIdentifier>
      <awardNumber awardURI="info:eu-repo/grantAgreement/EC/H2020/821890/">821890</awardNumber>
      <awardTitle>Retro Propulsion Assisted Landing Technologies</awardTitle>
    </fundingReference>
  </fundingReferences>
</resource>
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