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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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  <dc:creator>Vos, Jan</dc:creator>
  <dc:creator>Charbonnier, Dominique</dc:creator>
  <dc:creator>Marwege, Ansgar</dc:creator>
  <dc:creator>Guelhan Ali</dc:creator>
  <dc:creator>Laureti, Mariasole</dc:creator>
  <dc:creator>Karl, Sebastian</dc:creator>
  <dc:date>2022-01-05</dc:date>
  <dc:description>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 Göttingen. This paper provides a detailed comparison of Wind Tunnel Experiments with CFD calculations in the hypersonic regime, with and without retro propulsion.</dc:description>
  <dc:identifier>https://zenodo.org/record/5814915</dc:identifier>
  <dc:identifier>10.2514/6.2022-1308</dc:identifier>
  <dc:identifier>oai:zenodo.org:5814915</dc:identifier>
  <dc:relation>info:eu-repo/grantAgreement/EC/H2020/821890/</dc:relation>
  <dc:relation>url:https://zenodo.org/communities/retalt</dc:relation>
  <dc:rights>info:eu-repo/semantics/openAccess</dc:rights>
  <dc:rights>https://creativecommons.org/licenses/by/4.0/legalcode</dc:rights>
  <dc:title>Aerodynamic investigations of a Vertical Landing Launcher configuration by means of Computational Fluid Dynamics and Wind Tunnel Tests</dc:title>
  <dc:type>info:eu-repo/semantics/conferencePaper</dc:type>
  <dc:type>publication-conferencepaper</dc:type>
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