Oschwald, M. und Cuoco, F. und Yang, B. und De Rosa, M. (2005) Atomization and Combustion in LOX/H2- and LOX/CH4-Spray Flames. International Symposium on Heat and Mass Transfer in Spray Systems, 2005-06-05 - 2005-06-10, Anatalya (Turkey).
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Kurzfassung
Propellant injectors are for several reasons of central importance for the performance of rocket combustors. Existing correlations used to guide the design of injectors are mainly based on experimental und theoretical investigations of non-reacting sprays. Furthermore most of the experiments have been done with substitute fluids of significantly different properties as compared to liquid oxygen. Experimental investigations of reactive sprays with original propellants, liquid oxygen as oxidizer and hydrogen and methane as fuels, are presented and the influence of the injection conditions and of the fuel on the atomization and spray flame is discussed.
elib-URL des Eintrags: | https://elib.dlr.de/53333/ | ||||||||||||||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag, Paper) | ||||||||||||||||||||
Titel: | Atomization and Combustion in LOX/H2- and LOX/CH4-Spray Flames | ||||||||||||||||||||
Autoren: |
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Datum: | 2005 | ||||||||||||||||||||
Open Access: | Ja | ||||||||||||||||||||
Gold Open Access: | Nein | ||||||||||||||||||||
In SCOPUS: | Nein | ||||||||||||||||||||
In ISI Web of Science: | Nein | ||||||||||||||||||||
Status: | veröffentlicht | ||||||||||||||||||||
Stichwörter: | rocket propulsion | ||||||||||||||||||||
Veranstaltungstitel: | International Symposium on Heat and Mass Transfer in Spray Systems | ||||||||||||||||||||
Veranstaltungsort: | Anatalya (Turkey) | ||||||||||||||||||||
Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
Veranstaltungsbeginn: | 5 Juni 2005 | ||||||||||||||||||||
Veranstaltungsende: | 10 Juni 2005 | ||||||||||||||||||||
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 - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (alt) | ||||||||||||||||||||
Standort: | Lampoldshausen | ||||||||||||||||||||
Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Technologie | ||||||||||||||||||||
Hinterlegt von: | Oschwald, Dr.rer.nat. Michael | ||||||||||||||||||||
Hinterlegt am: | 16 Feb 2008 | ||||||||||||||||||||
Letzte Änderung: | 24 Apr 2024 19:16 |
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