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Lüdeke, Heinrich and Mulot, Jean Daniel and Hannemann, Klaus (2015) Launch Vehicle Base Flow Analysis Using Improved Delayed Detached Eddy Simulation. AIAA Journal, 53 (9), pp. 2454-2471. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J053297. ISSN 0001-1452.
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Official URL: http://arc.aiaa.org/doi/abs/10.2514/1.J053297
Abstract
During the ascent of carrier rockets the massively separated flow in the base region generates highly unsteady wall pressure fluctuations. The resulting dynamic loads can induce a response of the launcher structure called buffeting. In order to study the characteristics of the base flow behind three different configurations of the Ariane~5 launcher, Improved Delayed Detached Eddy Simulation (IDDES) in combination with unstructured grids is used. The objective of this work is to demonstrate the ability of IDDES to describe the impact of the connecting struts between central stage and boosters and to analyze the efficiency of a buffeting reduction device in the base region. Comparisons of the numerical results with time resolved and time averaged surface pressure data and PIV measurements obtained from the DNW High Speed Wind Tunnel are carried out in good agreement.
| Item URL in elib: | https://elib.dlr.de/99930/ | ||||||||||||||||
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| Document Type: | Article | ||||||||||||||||
| Title: | Launch Vehicle Base Flow Analysis Using Improved Delayed Detached Eddy Simulation | ||||||||||||||||
| Authors: |
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| Date: | 23 July 2015 | ||||||||||||||||
| Journal or Publication Title: | AIAA Journal | ||||||||||||||||
| Refereed publication: | Yes | ||||||||||||||||
| Open Access: | No | ||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||
| In SCOPUS: | Yes | ||||||||||||||||
| In ISI Web of Science: | Yes | ||||||||||||||||
| Volume: | 53 | ||||||||||||||||
| DOI: | 10.2514/1.J053297 | ||||||||||||||||
| Page Range: | pp. 2454-2471 | ||||||||||||||||
| Publisher: | American Institute of Aeronautics and Astronautics (AIAA) | ||||||||||||||||
| ISSN: | 0001-1452 | ||||||||||||||||
| Status: | Published | ||||||||||||||||
| Keywords: | computational fluid dynamics (CFD), improved delayed detached eddy simulation (IDDES), launch vehicle base flow, base buffeting, buffeting reduction device | ||||||||||||||||
| 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 , Göttingen | ||||||||||||||||
| Institutes and Institutions: | Institute of Aerodynamics and Flow Technology > Transport Aircraft Institute of Aerodynamics and Flow Technology > Spacecraft | ||||||||||||||||
| Deposited By: | Lüdeke, Dr.-Ing. Heinrich | ||||||||||||||||
| Deposited On: | 25 Nov 2015 10:19 | ||||||||||||||||
| Last Modified: | 28 Nov 2023 08:32 |
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