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Computational fluid dynamics investigations of aerodynamic control surfaces of a vertical landing configuration

Charbonnier, Dominique and Vos, Jan and Marwege, Ansgar and Hantz, Christian (2022) Computational fluid dynamics investigations of aerodynamic control surfaces of a vertical landing configuration. CEAS Space Journal, 14 (3), pp. 517-532. Springer. doi: 10.1007/s12567-022-00431-6. ISSN 1868-2502.

Full text not available from this repository.

Official URL: https://doi.org/10.1007/s12567-022-00431-6

Abstract

The European project RETALT (Retro Propulsion Assisted Landing Technologies), funded by the Horizon 2020 framework program (Grant agreement No 821890), has as main objective to investigate critical technologies for the assisted descent and landing of re-usable first stages. Among these technologies, one can find aerodynamics, aerothermodynamics, flight dynamics, guidance navigation and control (GNC), Structures, mechanisms, thrust vector control (TVC) and thermal protection systems (TPS). The present paper focuses in particularly on the aerodynamics technology applied to a vertical landing launcher configuration, called RETALT1, including retro-propulsion. During the landing phase of the first stage of the launcher, the main devices for control and trim of the vehicle (besides the retro-propulsion) are the aerodynamic control surfaces (ACS). Three types of aerodynamic control surfaces are investigated by means of numerical computations, using the NSMB (Navier Stokes Multi Block) CFD code. The control surfaces considered are the deployable interstage segments (also named petals), grid fins and planar fins. Aerodynamic coefficients as well as forces acting on the control surfaces are extracted from the CFD computations to assess the efficiency of each type of devices and to populate the Aerodynamic Database (AEDB) for flight dynamic analysis.

Item URL in elib:https://elib.dlr.de/188193/
Document Type:Article
Title:Computational fluid dynamics investigations of aerodynamic control surfaces of a vertical landing configuration
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Charbonnier, DominiqueCFSEhttps://orcid.org/0000-0002-9600-9258UNSPECIFIED
Vos, JanCFS Engineeringhttps://orcid.org/0000-0003-1525-943XUNSPECIFIED
Marwege, AnsgarUNSPECIFIEDhttps://orcid.org/0000-0002-3912-9114UNSPECIFIED
Hantz, ChristianUNSPECIFIEDhttps://orcid.org/0000-0002-6911-6410UNSPECIFIED
Date:25 March 2022
Journal or Publication Title:CEAS Space Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:14
DOI:10.1007/s12567-022-00431-6
Page Range:pp. 517-532
Publisher:Springer
Series Name:Special Issue on Retro propulsion assisted landing technologies: the RETALT project
ISSN:1868-2502
Status:Published
Keywords:Aerodynamic, CFD, Control Surface, Reusable Launcher, Vertical Landing
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 - Reusable Space Systems and Propulsion Technology
Location: Köln-Porz
Institutes and Institutions:Institute for Aerodynamics and Flow Technology > Supersonic and Hypersonic Technology
Deposited By: Marwege, Ansgar
Deposited On:22 Nov 2022 09:20
Last Modified:27 Mar 2023 10:09

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