elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Contact | Deutsch
Fontsize: [-] Text [+]

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 Verlag. 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

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 Authors
Hannemann, KlausUNSPECIFIED
Karl, SebastianUNSPECIFIED
Martinez Schramm, JanUNSPECIFIED
Steelant, JohanESA-ESTEC, Noordwijk
Date:11 August 2010
Journal or Publication Title:Shock Waves
Refereed publication:Yes
In 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 Verlag
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: Dagmar Brennecke-Hosseinzadeh
Deposited On:08 Oct 2010 09:07
Last Modified:04 Apr 2013 16:23

Repository Staff Only: item control page

Browse
Search
Help & Contact
Informationen
electronic library is running on EPrints 3.3.12
Copyright © 2008-2012 German Aerospace Center (DLR). All rights reserved.