Hardi, Justin und Oschwald, Michael (2013) Cryogenic oxygen jet response to transverse acoustic excitation with 1T and 1L1T modes. In: Proceedings 5th EUCASS. 5th European Conference for Aeronautics and Space Sciences EUCASS 2013, 1. - 5. Jul. 2013, München, Germany. ISBN 978-84-941531-0-5.
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Kurzfassung
The intact length of the dense oxygen core from an oxygen-hydrogen, shear coaxial rocket injector was measured. The measurements were made in a rectangular rocket combustor with optical access and acoustic forcing. The combustor was operated at chamber pressures of 40 and 60 bar, with either ambient temperature or cryogenic hydrogen. The multi-element injection spray is subjected to forced transverse gas oscillations of two different acoustic resonance modes; the first transverse (1T) mode at 4200 Hz, and the first combined longitudinal-transverse (1L1T) at 5500 Hz. Intact core length is measured from high-speed shadowgraph imaging. The dependence of intact core length with increasing acoustic amplitude is compared for the two modes of excitation.
elib-URL des Eintrags: | https://elib.dlr.de/85312/ | ||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||
Titel: | Cryogenic oxygen jet response to transverse acoustic excitation with 1T and 1L1T modes | ||||||||||||
Autoren: |
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Datum: | 2013 | ||||||||||||
Erschienen in: | Proceedings 5th EUCASS | ||||||||||||
Referierte Publikation: | Ja | ||||||||||||
Open Access: | Nein | ||||||||||||
Gold Open Access: | Nein | ||||||||||||
In SCOPUS: | Nein | ||||||||||||
In ISI Web of Science: | Nein | ||||||||||||
ISBN: | 978-84-941531-0-5 | ||||||||||||
Status: | veröffentlicht | ||||||||||||
Stichwörter: | combustion; instability; cryogenic; jet; acoustics | ||||||||||||
Veranstaltungstitel: | 5th European Conference for Aeronautics and Space Sciences EUCASS 2013 | ||||||||||||
Veranstaltungsort: | München, Germany | ||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||
Veranstaltungsdatum: | 1. - 5. Jul. 2013 | ||||||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||
HGF - Programm: | Raumfahrt | ||||||||||||
HGF - Programmthema: | Raumtransport | ||||||||||||
DLR - Schwerpunkt: | Raumfahrt | ||||||||||||
DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | R - Antriebsystemtechnik - Schubkammertechnologie (alt) | ||||||||||||
Standort: | Lampoldshausen | ||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Raketenantriebe | ||||||||||||
Hinterlegt von: | Hanke, Michaela | ||||||||||||
Hinterlegt am: | 22 Nov 2013 09:19 | ||||||||||||
Letzte Änderung: | 01 Dez 2018 19:49 |
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