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Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths

Hannemann, Klaus and Karl, Sebastian and Martinez Schramm, Jan and Steelant, Johan (2010) Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths. Shock Waves, Vol. 20 (5), pp. 353-366. Springer. DOI: 10.1007/s00193-010-0269-8 ISSN 0938-1287

Full text not available from this repository.

Official URL: http://www.springer.com/engineering/mechanical+eng/journal/193

Abstract

In the framework of the European Commission co-funded LAPCAT (Long-Term Advanced Propulsion Concepts and Technologies) project, the methodology of a combined ground-based testing and numerical modelling analysis of supersonic combustion flow paths was established. The approach is based on free jet testing of complete supersonic combustion ramjet (scramjet) configurations consisting of intake, combustor and nozzle in the High Enthalpy Shock Tunnel Göttingen (HEG) of the German Aerospace Center (DLR) and computational fluid dynamics studies utilising the DLR TAU code. The capability of the established methodology is demonstrated by applying it to the flow path of the generic HyShot II scramjet flight experiment configuration

Item URL in elib:https://elib.dlr.de/65344/
Document Type:Article
Additional Information:Journal No. 193
Title:Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Hannemann, KlausUNSPECIFIEDUNSPECIFIED
Karl, SebastianUNSPECIFIEDUNSPECIFIED
Martinez Schramm, JanUNSPECIFIEDUNSPECIFIED
Steelant, JohanESA-ESTEC, NoordwijkUNSPECIFIED
Date:11 August 2010
Journal or Publication Title:Shock Waves
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:Vol. 20
DOI :10.1007/s00193-010-0269-8
Page Range:pp. 353-366
Publisher:Springer
ISSN:0938-1287
Status:Published
Keywords:Ground based testing · Computational fluid dynamics · Combustion modelling · Supersonic combustion ramjet · Short duration impulse facility · High enthalpy shock tunnel
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Grundlagen Raumtransport - Anlagen und Messtechnik (old)
Location: Göttingen
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Spacecraft
Deposited By: Brennecke-Hosseinzadeh, Dagmar
Deposited On:08 Oct 2010 09:07
Last Modified:10 Jan 2019 15:50

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