Fertig, Markus (2014) EXOMARS 2018 - DLR-CFD Activities Synthesis Report. Project Report. EXM-D2-TNO-DLR-0001. Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR). 60 S.
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Abstract
This document describes the DLR supersonic and hypersonic CFD activities performed in the frame of the EXOMARS 2018 project. Eighteen different flow conditions from the reference trajectory have been simulated employing the DLR CFD code TAU in order to determine the aerodynamic coefficients as well as heating rates at hypersonic speed of the EXOMARS 2018 vehicle. Two initial grids have been used in order to resolve the boundary layer and the surface conditions properly. All grids were adapted several times to obtain grid converged results. However, especially the surface heating results show some scatter which is based on the usage of unstructured grids. Therefore, smoothed heating results are shown in the report in addition.
Item URL in elib: | https://elib.dlr.de/95742/ | ||||||||
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Document Type: | Monograph (Project Report) | ||||||||
Title: | EXOMARS 2018 - DLR-CFD Activities Synthesis Report | ||||||||
Authors: |
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Date: | 30 July 2014 | ||||||||
Refereed publication: | No | ||||||||
Open Access: | No | ||||||||
Gold Open Access: | No | ||||||||
In SCOPUS: | No | ||||||||
In ISI Web of Science: | No | ||||||||
Number of Pages: | 60 | ||||||||
Status: | Published | ||||||||
Keywords: | atmospheric entry, Mars | ||||||||
Institution: | Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR) | ||||||||
Department: | Institut für Aerodynamik und Strömungstechnik, Abteilung Raumfahrzeuge | ||||||||
HGF - Research field: | Aeronautics, Space and Transport | ||||||||
HGF - Program: | Space | ||||||||
HGF - Program Themes: | Space Transportation | ||||||||
DLR - Research area: | Raumfahrt | ||||||||
DLR - Program: | R RP - Space Transportation | ||||||||
DLR - Research theme (Project): | R - Raumfahrzeugsysteme - Numerische Verfahren und Simulation (old) | ||||||||
Location: | Braunschweig | ||||||||
Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Spacecraft | ||||||||
Deposited By: | Fertig, Dr. Markus | ||||||||
Deposited On: | 25 Mar 2015 14:10 | ||||||||
Last Modified: | 01 Dec 2018 19:51 |
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