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Oschwald, M. and Cuoco, F. and Yang, B. and 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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Abstract
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.
| Item URL in elib: | https://elib.dlr.de/53333/ | ||||||||||||||||||||
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| Document Type: | Conference or Workshop Item (Speech, Paper) | ||||||||||||||||||||
| Title: | Atomization and Combustion in LOX/H2- and LOX/CH4-Spray Flames | ||||||||||||||||||||
| Authors: |
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| Date: | 2005 | ||||||||||||||||||||
| Open Access: | Yes | ||||||||||||||||||||
| Gold Open Access: | No | ||||||||||||||||||||
| In SCOPUS: | No | ||||||||||||||||||||
| In ISI Web of Science: | No | ||||||||||||||||||||
| Status: | Published | ||||||||||||||||||||
| Keywords: | rocket propulsion | ||||||||||||||||||||
| Event Title: | International Symposium on Heat and Mass Transfer in Spray Systems | ||||||||||||||||||||
| Event Location: | Anatalya (Turkey) | ||||||||||||||||||||
| Event Type: | international Conference | ||||||||||||||||||||
| Event Start Date: | 5 June 2005 | ||||||||||||||||||||
| Event End Date: | 10 June 2005 | ||||||||||||||||||||
| 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 - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old) | ||||||||||||||||||||
| Location: | Lampoldshausen | ||||||||||||||||||||
| Institutes and Institutions: | Institute of Space Propulsion > Technologie | ||||||||||||||||||||
| Deposited By: | Oschwald, Dr.rer.nat. Michael | ||||||||||||||||||||
| Deposited On: | 16 Feb 2008 | ||||||||||||||||||||
| Last Modified: | 24 Apr 2024 19:16 |
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