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Hannemann, Klaus und Karl, Sebastian und Martinez Schramm, Jan und Steelant, Johan (2010) Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths. Shock Waves, Vol. 20 (5), Seiten 353-366. Springer. doi: 10.1007/s00193-010-0269-8. ISSN 0938-1287.
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Offizielle URL: http://www.springer.com/engineering/mechanical+eng/journal/193
Kurzfassung
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
| elib-URL des Eintrags: | https://elib.dlr.de/65344/ | ||||||||||||||||||||
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| Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||
| Zusätzliche Informationen: | Journal No. 193 | ||||||||||||||||||||
| Titel: | Methodology of a combined ground based testing and numerical modelling analysis of supersonic combustion flow paths | ||||||||||||||||||||
| Autoren: |
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| Datum: | 11 August 2010 | ||||||||||||||||||||
| Erschienen in: | Shock Waves | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||
| In ISI Web of Science: | Ja | ||||||||||||||||||||
| Band: | Vol. 20 | ||||||||||||||||||||
| DOI: | 10.1007/s00193-010-0269-8 | ||||||||||||||||||||
| Seitenbereich: | Seiten 353-366 | ||||||||||||||||||||
| Verlag: | Springer | ||||||||||||||||||||
| ISSN: | 0938-1287 | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | Ground based testing · Computational fluid dynamics · Combustion modelling · Supersonic combustion ramjet · Short duration impulse facility · High enthalpy shock tunnel | ||||||||||||||||||||
| HGF - Forschungsbereich: | Verkehr und Weltraum (alt) | ||||||||||||||||||||
| HGF - Programm: | Weltraum (alt) | ||||||||||||||||||||
| HGF - Programmthema: | W RP - Raumtransport | ||||||||||||||||||||
| DLR - Schwerpunkt: | Weltraum | ||||||||||||||||||||
| DLR - Forschungsgebiet: | W RP - Raumtransport | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | W - Grundlagen Raumtransport - Anlagen und Messtechnik (alt) | ||||||||||||||||||||
| Standort: | Göttingen | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Aerodynamik und Strömungstechnik > Raumfahrzeuge | ||||||||||||||||||||
| Hinterlegt von: | Brennecke-Hosseinzadeh, Dagmar | ||||||||||||||||||||
| Hinterlegt am: | 08 Okt 2010 09:07 | ||||||||||||||||||||
| Letzte Änderung: | 10 Jan 2019 15:50 |
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