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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.
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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/ | ||||||||||||||||||||
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| 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: |
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| 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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