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HyperCODA -- Extension of Flow Solver CODA towards Hypersonic Flows

Huismann, Immo and Fechter, Stefan and Leicht, Tobias (2021) HyperCODA -- Extension of Flow Solver CODA towards Hypersonic Flows. In: 22nd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIII, 151, pp. 99-109. Springer International Publishing. STAB-Symposium 2020, Germany. doi: 10.1007/978-3-030-79561-0_10. ISBN 978-3-030-79560-3. ISSN 1612-2909.

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Official URL: https://link.springer.com/chapter/10.1007/978-3-030-79561-0_10

Abstract

This paper presents HyperCODA, the hypersonics extension to the flow solver CODA (CFD for ONERA, DLR and Airbus). Similar to the spacecraft extensions of TAU, HyperCODA extends CODA for applications at high Mach numbers, including non-ideal gas thermodynamics, gas mixtures, and chemistry. The paper discusses simulations demonstrating numerical convergence and stability properties, as well as a supersonic rocket retropropulsion maneuver. Cross-code comparisons are made against the established DLR TAU code.

Item URL in elib:https://elib.dlr.de/140866/
Document Type:Conference or Workshop Item (Other)
Title:HyperCODA -- Extension of Flow Solver CODA towards Hypersonic Flows
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Huismann, ImmoImmo.Huismann (at) dlr.deUNSPECIFIED
Fechter, StefanStefan.Fechter (at) dlr.dehttps://orcid.org/0000-0002-8439-8786
Leicht, TobiasTobias.Leicht (at) dlr.deUNSPECIFIED
Date:14 July 2021
Journal or Publication Title:22nd STAB/DGLR Symposium on New Results in Numerical and Experimental Fluid Mechanics XIII
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
Volume:151
DOI :10.1007/978-3-030-79561-0_10
Page Range:pp. 99-109
Editors:
EditorsEmailEditor's ORCID iD
Dillmann, AndreasAndreas.Dillmann@dlr.deUNSPECIFIED
Heller, GerdAirbus BremenUNSPECIFIED
Wagner, ClausClaus.Wagner@dlr.deUNSPECIFIED
Publisher:Springer International Publishing
Series Name:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ISSN:1612-2909
ISBN:978-3-030-79560-3
Status:Published
Keywords:CFD, hypersonic flow, finite volume method, numerical software
Event Title:STAB-Symposium 2020
Event Location:Germany
Event Type:national Conference
Organizer:Die Deutsche Strömungsmechanische Arbeitsgemeinschaft, STAB
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:fixed-wing aircraft
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Simulation and Validation (old)
Location: Dresden
Institutes and Institutions:Institute of Software Methods for Product Virtualization > High Perfomance Computing
Institute for Aerodynamics and Flow Technology > Spacecraft, GO
Institute for Aerodynamics and Flow Technology > CASE, BS
Deposited By: Huismann, Immo
Deposited On:09 Aug 2021 14:46
Last Modified:15 Mar 2022 15:34

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