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Numerical Investigation of a 7-Element GOX / GCH 4 Subscale Combustion Chamber
| Content Provider | Semantic Scholar |
|---|---|
| Author | Eiringhaus, Daniel Rahn, Daniel Riedmann, Hendrik Knab, Oliver Haidn, Oskar |
| Copyright Year | 2017 |
| Abstract | For future liquid rocket engines methane has become the focus of several studies on alternative fuels in the western hemisphere. At ArianeGroup numerical simulation tools have been established as a powerful instrument in the design process. In order to achieve the same confidence level for CH4/O2 as for H2/O2 combustion, the applied numerical models have to be adapted and validated against sufficient test data. At the Chair of Space Propulsion at the Technical University of Munich (TUM) several combustion chambers have been designed and tests at different operating points have been conducted. In this paper one of these subscale combustion chambers with calorimetric cooling and seven shear coaxial injection elements running on gaseous methane and oxygen is used to examine ArianeGroup’s in-house tools for combustion chamber performance analysis. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | https://www.eucass.eu/doi/EUCASS2017-173.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
