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Zeriadtke, Jan Erik (2023) Abbrandsimulationen von Hybridraketentriebwerken mittels impliziter Geometriebeschreibungen. Student thesis, Technische Universität Braunschweig.
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| Item URL in elib: | https://elib.dlr.de/197528/ | ||||||||
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| Document Type: | Thesis (Student thesis) | ||||||||
| Title: | Abbrandsimulationen von Hybridraketentriebwerken mittels impliziter Geometriebeschreibungen | ||||||||
| Authors: |
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| Date: | 2023 | ||||||||
| Refereed publication: | No | ||||||||
| Open Access: | No | ||||||||
| Gold Open Access: | No | ||||||||
| In SCOPUS: | No | ||||||||
| In ISI Web of Science: | No | ||||||||
| Number of Pages: | 71 | ||||||||
| Status: | Published | ||||||||
| Keywords: | Abbrandsimulation, implizite Oberfläche, Signed Distance Function, Brennstoffblock und Hybridrakete | ||||||||
| Institution: | Technische Universität Braunschweig | ||||||||
| Department: | Fakultät für Maschinenbau | ||||||||
| 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 - Reusable Space Systems and Propulsion Technology | ||||||||
| Location: | Braunschweig | ||||||||
| Institutes and Institutions: | Institute for Aerodynamics and Flow Technology > Spacecraft, BS | ||||||||
| Deposited By: | Passern, Silke | ||||||||
| Deposited On: | 02 Nov 2023 11:06 | ||||||||
| Last Modified: | 02 Nov 2023 11:06 |
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