Karl, Sebastian and Markus, Lambert (2009) CFD modeling of hypervelocity re-entry flows including gas radiation. 27th International Symposium on Shock Waves, 19.-24. Juli 2009, St. Petersburg (Russia).
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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 modeling. This paper describes a Monte-Carlo based method to solve the radiative transfer equation. The resulting energy sources are coupled to a CFD solver to account for the additional mechanism of radiative energy transport. This approach is validated using a canonical test problem and applied to the FIRE II flight experiment configuration.
|Document Type:||Conference or Workshop Item (Speech, Paper)|
|Title:||CFD modeling of hypervelocity re-entry flows including gas radiation|
|Keywords:||Radiation, CFD, re-entry, Aerothermodynamics|
|Event Title:||27th International Symposium on Shock Waves|
|Event Location:||St. Petersburg (Russia)|
|Event Type:||international Conference|
|Event Dates:||19.-24. Juli 2009|
|Organizer:||ISWI International Shock Wave Institute|
|HGF - Research field:||other|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||W - Grundlagen Raumtransport - numerische Verfahren (old)|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Spacecraft|
Institute of Aerodynamics and Flow Technology > CASE
|Deposited By:||Sebastian Karl|
|Deposited On:||25 Nov 2009 09:59|
|Last Modified:||26 Nov 2009 14:34|
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