elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Impressum | Datenschutz | Kontakt | English
Schriftgröße: [-] Text [+]

Advanced Ablation Characterization and Modelling

Gülhan, Ali (2016) Advanced Ablation Characterization and Modelling. 8th European Workshop on Thermal Protection Systems and Hot Structures, 19.-22. Apr. 2016, Noordwijk, Niederlande.

Dieses Archiv kann nicht den Volltext zur Verfügung stellen.

Kurzfassung

Ablative thermal protection materials are a key technology for current and future space exploration missions. However, the mission feasibility is determined by the materials available, and the development of new materials is performed, essentially, by an iterative trial-and-error process. This is due to the absence of validated predictive models for ablative material behaviour. Models are tuned to bulk material properties from tests. In order to describe physical processes of the ablation correctly, the European FP7 project ABLAMOD with the partner organizations DLR, Airbus Defence&Space, Avio, Amoroim, Fluid Gravity Engineering, AIT, OGI, CIRA, VKI and University of Strathclyde has been formed. The main objective of the ABLAMOD project is to make a substantial step towards a predictive model of an ablative thermal protection system by incorporating aspects of high fidelity mesoscale ablator physics within a modular framework. In order to successfully develop such physics modules, the understanding of the fundamental processes occurring within the ablative materials must be improved. To this end, three major ablation materials, i.e. carbon based, silicon based and cork based ablators, need to be tested in well characterized long duration high enthalpy facilities using both standard instrumentation and advanced measurement techniques. These advanced spectroscopic techniques lead to a significant improvement in the detailed characterisation of the material behaviour at the mesoscale level. Both virgin and char versions of the materials have been thermally characterized and the internal structure has been scanned by means of Computer Tomography (CT). In parallel using the state-of-the-art knowledge of ablator physical processes, modules for the specific phenomena like internal gas flow, radiation, gas transport properties and gas-surface interaction have been developed. Computed Pitot pressure and heat flux profiles using simplified thermal non-equilibrium model show a good agreement with the experimental data in the arc heated facility L3K. The computer tomography data allowed studying the microstructure of all three ablator materials before and after charring. This data has been directly used for DSMC modelling. A high enthalpy flow field has been simulated using a Computational Fluid Dynamics (CFD) code. This simulation used updated transport properties of the gas. The results of numerical rebuilding of the thermal response of the carbon based ablation material using the ablation code FABL in combination with the new modules developed within the ABLAMOD project showed an improved agreement with experimental data.

elib-URL des Eintrags:https://elib.dlr.de/110296/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Advanced Ablation Characterization and Modelling
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Gülhan, AliAli.Guelhan (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:April 2016
Referierte Publikation:Nein
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Nein
In ISI Web of Science:Nein
Status:veröffentlicht
Stichwörter:Ablation, thermal protection, ABLAMOD
Veranstaltungstitel:8th European Workshop on Thermal Protection Systems and Hot Structures
Veranstaltungsort:Noordwijk, Niederlande
Veranstaltungsart:Workshop
Veranstaltungsdatum:19.-22. Apr. 2016
Veranstalter :European Space Agency (ESA)
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Raumfahrt
HGF - Programmthema:Raumtransport
DLR - Schwerpunkt:Raumfahrt
DLR - Forschungsgebiet:R RP - Raumtransport
DLR - Teilgebiet (Projekt, Vorhaben):R - EU Projekte Raumtransport (alt)
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Aerodynamik und Strömungstechnik > Über- und Hyperschalltechnologien
Hinterlegt von: Willems, Sebastian
Hinterlegt am:06 Jan 2017 11:31
Letzte Änderung:20 Jun 2021 15:48

Nur für Mitarbeiter des Archivs: Kontrollseite des Eintrags

Blättern
Suchen
Hilfe & Kontakt
Informationen
electronic library verwendet EPrints 3.3.12
Gestaltung Webseite und Datenbank: Copyright © Deutsches Zentrum für Luft- und Raumfahrt (DLR). Alle Rechte vorbehalten.