Karl, Sebastian and Lambert, Markus (2011) CFD Modelling of Re-entry Flows including Gas Radiation. 7th European Aerothermodynamics Symposium, 09.-12. May 2011, Brugge, Belgium.
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Space exploration missions may include atmospheric entries at high velocities (e.g. sample-return, hyperbolic entries) or into an atmosphere with highly radiative constituents (e.g. Jupiter, Titan). The energy transport by gas radiation can become significant at such flow conditions and requires adequate modelling. This paper describes results of a CFD study of the FIRE II and Huygens fore-body flow at peak heating conditions including radiation effects employing a loose coupling strategy between the flow and radiation solvers.
|Document Type:||Conference or Workshop Item (Speech, Paper)|
|Title:||CFD Modelling of Re-entry Flows including Gas Radiation|
|In ISI Web of Science:||No|
|Series Name:||Conference Proceedings|
|Keywords:||CFD, Radiation, Reentry, Aerothermochemistry|
|Event Title:||7th European Aerothermodynamics Symposium|
|Event Location:||Brugge, Belgium|
|Event Type:||international Conference|
|Event Dates:||09.-12. May 2011|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||W - Raumfahrzeugsysteme - Numerische Verfahren und Simulation (old)|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Spacecraft|
|Deposited By:||Sebastian Karl|
|Deposited On:||21 Nov 2011 14:30|
|Last Modified:||21 Nov 2011 14:30|
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