Martin, Jan und Nakaya, Shinji und Börner, Michael und Hardi, Justin (2025) Nonlinear mode decomposition of unsteady LOX/LNG flame imaging in an optically accessible rocket combustor. In: 35th International Symposium on Space Technology and Science ISTS. 35th International Symposium on Space Technology and Science ISTS, 2025-07-12 - 2025-07-18, Tokushima, Japan.
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Kurzfassung
Combustion instabilities are characterized by nonlinear dynamics changing on short timescales. Common multivariable data analysis approaches like Dynamic Mode Decomposition linearise the underlying data source. The Koopman theory states that with a suitable transformation each nonlinear system can be linearly mapped with the Koopman operator. A variational autoencoder was trained in this work to approximate the Koopman operator along with the necessary transformation. This enabled analysis of nonlinear and time-varying effects in the radiation imaging of the flame in a LOX/LNG rocket combustor and the corresponding unsteady pressure data. In contrast to reconstructed DMD modes, the Koopman netwtwork provided a time resolved development of the underlying dynamics in the interaction between hydrodynamics and thermoacoustics in the development of combustion instabilities.
| elib-URL des Eintrags: | https://elib.dlr.de/218743/ | ||||||||||||||||||||
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| Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||||||||||||||
| Titel: | Nonlinear mode decomposition of unsteady LOX/LNG flame imaging in an optically accessible rocket combustor | ||||||||||||||||||||
| Autoren: |
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| Datum: | Juli 2025 | ||||||||||||||||||||
| Erschienen in: | 35th International Symposium on Space Technology and Science ISTS | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Nein | ||||||||||||||||||||
| Gold Open Access: | Nein | ||||||||||||||||||||
| In SCOPUS: | Nein | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | rocket engine, optical access, liquid oxygen / natural gas, single-injector, dynamic mode decomposition, nonlinear mode decomposition | ||||||||||||||||||||
| Veranstaltungstitel: | 35th International Symposium on Space Technology and Science ISTS | ||||||||||||||||||||
| Veranstaltungsort: | Tokushima, Japan | ||||||||||||||||||||
| Veranstaltungsart: | internationale Konferenz | ||||||||||||||||||||
| Veranstaltungsbeginn: | 12 Juli 2025 | ||||||||||||||||||||
| Veranstaltungsende: | 18 Juli 2025 | ||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
| HGF - Programm: | Raumfahrt | ||||||||||||||||||||
| HGF - Programmthema: | Raumtransport | ||||||||||||||||||||
| DLR - Schwerpunkt: | Raumfahrt | ||||||||||||||||||||
| DLR - Forschungsgebiet: | R RP - Raumtransport | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | R - Wiederverwendbare Raumfahrtsysteme und Antriebstechnologie | ||||||||||||||||||||
| Standort: | Lampoldshausen | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Raumfahrtantriebe > Raketenantriebstechnologie | ||||||||||||||||||||
| Hinterlegt von: | Martin, Jan | ||||||||||||||||||||
| Hinterlegt am: | 11 Nov 2025 11:10 | ||||||||||||||||||||
| Letzte Änderung: | 11 Nov 2025 11:10 |
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