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Trotta, Luca (2022) Aeroacoustic modeling of a LOX/CH4 rocket engine for high-frequency combustion instability prediction analyses. Master's, Delft University of Technology.
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| Item URL in elib: | https://elib.dlr.de/192048/ | ||||||||
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| Document Type: | Thesis (Master's) | ||||||||
| Title: | Aeroacoustic modeling of a LOX/CH4 rocket engine for high-frequency combustion instability prediction analyses | ||||||||
| Authors: |
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| Date: | 30 November 2022 | ||||||||
| Refereed publication: | Yes | ||||||||
| Open Access: | No | ||||||||
| Status: | Published | ||||||||
| Keywords: | LUMEN, combustion instabilities, thermoacoustics, acoustic modelling, linearized Navier Stokes (LNS) simulation | ||||||||
| Institution: | Delft University of Technology | ||||||||
| Department: | Faculty of Aerospace Engineering | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | Space | ||||||||
| HGF - Program Themes: | Space Transportation | ||||||||
| DLR - Research area: | Raumfahrt | ||||||||
| DLR - Program: | R RP - Space Transportation | ||||||||
| DLR - Research theme (Project): | R - Project LUMEN (Liquid Upper Stage Demonstrator Engine) | ||||||||
| Location: | Lampoldshausen | ||||||||
| Institutes and Institutions: | Institute of Space Propulsion > Rocket Propulsion Technology | ||||||||
| Deposited By: | Böhringer, Isabell | ||||||||
| Deposited On: | 12 Dec 2022 09:58 | ||||||||
| Last Modified: | 12 Dec 2022 09:58 |
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