Alff, F. und Böhm, M, und Clauß, W. und Oschwald, M. und Waidmann, W. (1994) Supersonic Combustion of Hydrogen/Air in a Scramjet Combustion Chamber. 45th International Astronautical Congress; 9th - 14th Oct., 1994; Jerusalem; Israel.
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Kurzfassung
Due to the importance of supersonic combustion in hypersonic propulsion an experimental investigation of the flowfield of a supersonic ramjet combustion chamber (scramjet) at a Mach number of 2 has been carried out. The simulated free flight Mach number was about 5. The hydrogen was injected parallel to the air stream throughthe base of a symmetric wedge (strut) centered in the two dimensionalcombustion chamber. The strut served as a flameholder. Spontaneous OH-emission, schlieren photography and pitot pressure measurements were used to acquire basic information about the flowfield. Quantitativ measurements were made with a 2D Laser-Doppler- Velocimeter (LDV) from which the mean velocity, turbulent intensitiesand Reynolds stresses were determined. Coherent-Anti-Stokes-Raman- Scattering (CARS) was used to determine the temperature histograms for each measurement point. The histrograms show the turbulent temperature fluctuations in the combustion chamber.
elib-URL des Eintrags: | https://elib.dlr.de/24813/ | ||||||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Paper) | ||||||||||||||||||||||||
Zusätzliche Informationen: | institution=IAF, LIDO-Berichtsjahr=1994, pages=10, | ||||||||||||||||||||||||
Titel: | Supersonic Combustion of Hydrogen/Air in a Scramjet Combustion Chamber. | ||||||||||||||||||||||||
Autoren: |
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Datum: | 1994 | ||||||||||||||||||||||||
Open Access: | Nein | ||||||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||||||
Name der Reihe: | IAF 94-S.4.429 | ||||||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||||||
Veranstaltungstitel: | 45th International Astronautical Congress; 9th - 14th Oct., 1994; Jerusalem; Israel | ||||||||||||||||||||||||
HGF - Forschungsbereich: | NICHT SPEZIFIZIERT | ||||||||||||||||||||||||
HGF - Programm: | keine Zuordnung | ||||||||||||||||||||||||
HGF - Programmthema: | keine Zuordnung | ||||||||||||||||||||||||
DLR - Schwerpunkt: | NICHT SPEZIFIZIERT | ||||||||||||||||||||||||
DLR - Forschungsgebiet: | keine Zuordnung | ||||||||||||||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | NICHT SPEZIFIZIERT | ||||||||||||||||||||||||
Standort: | Lampoldshausen | ||||||||||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Institut für Chemische Antriebe und Verfahrenstechnik | ||||||||||||||||||||||||
Hinterlegt von: | DLR-Beauftragter, elib | ||||||||||||||||||||||||
Hinterlegt am: | 02 Apr 2006 | ||||||||||||||||||||||||
Letzte Änderung: | 27 Apr 2009 05:35 |
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