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Comparison of different modeling approaches for CFD simulations of a single-element GCH 4 / GOX rocket combustor
| Content Provider | Semantic Scholar |
|---|---|
| Author | Roth, Christine-Andrea Haidn, Oskar Riedmann, H. Ivancic, B. Maestro, Del Cuenot, Bénédicte Selle, Laurent Daimon, Yu Chemnitz, Alexander Keller, R. Zips, Julian Frank, G. Müller, Heiner |
| Copyright Year | 2015 |
| Abstract | As part of the Combustion Modeling Workshop during the SFB/TRR 40 Summer Program 2015 at the Technische Universität München, numerical simulations of flow and combustion in a single-element GCH4/GOX rocket combustor have been performed using different modeling approaches implemented in different computational tools. The differences and commonalities between these approaches and tools are outlined in this report. The results obtained with the different tools for a common operating point are presented. They show large discrepancies in the prediction of relevant validation and design parameters. The causes for these discrepancies are discussed. In addition the numerical results are compared to the experimental data obtained at the Institute for Flight Propulsion at the Technische Universität München for the simulated operating point. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | http://www.sfbtr40.de/fileadmin/Summer_Programs/Summer_Program_2015/summer-program-2015-08.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |
