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Montano Rejas, Zhuzhell und Seidler, Marcel und Riemenschneider, Johannes und Friedrichs, Jens (2022) A Coupling Method for the Design of Shape-Adaptive Compressor Blades. Applied Mechanics, 3 (1), Seiten 182-209. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/applmech3010014. ISSN 2673-3161.
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Offizielle URL: https://www.mdpi.com/2673-3161/3/1/14
Kurzfassung
The design of flexible and efficient propulsion systems is crucial for the development of future low-emission aircraft. Applying shape-adaptive blades in jet engine compressors presents a high potential for increasing efficiency, since such blades are capable of adapting to different flight phases and aerodynamic conditions. Such blade morphing behavior can be achieved through structurally integrated actuation. Since no morphing aircraft engine blades exist to date, a multidisciplinary method for their design is introduced. This new method brings together existing structural and aerodynamic design methodologies, couples them already at the earliest stages of the design process, and addresses the challenges of such a tightly coupled multidisciplinary design approach.
| elib-URL des Eintrags: | https://elib.dlr.de/186131/ | ||||||||||||||||||||
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| Dokumentart: | Zeitschriftenbeitrag | ||||||||||||||||||||
| Zusätzliche Informationen: | We would like to acknowledge the funding by the Deutsche Forschungsgemeinschaft (DFG, German Research Foundation) under Germany´s Excellence Strategy—EXC 2163/1- Sustainable and Energy Efficient Aviation—Project-ID 390881007 | ||||||||||||||||||||
| Titel: | A Coupling Method for the Design of Shape-Adaptive Compressor Blades | ||||||||||||||||||||
| Autoren: |
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| Datum: | 11 Februar 2022 | ||||||||||||||||||||
| Erschienen in: | Applied Mechanics | ||||||||||||||||||||
| Referierte Publikation: | Ja | ||||||||||||||||||||
| Open Access: | Ja | ||||||||||||||||||||
| Gold Open Access: | Ja | ||||||||||||||||||||
| In SCOPUS: | Ja | ||||||||||||||||||||
| In ISI Web of Science: | Nein | ||||||||||||||||||||
| Band: | 3 | ||||||||||||||||||||
| DOI: | 10.3390/applmech3010014 | ||||||||||||||||||||
| Seitenbereich: | Seiten 182-209 | ||||||||||||||||||||
| Herausgeber: |
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| Verlag: | Multidisciplinary Digital Publishing Institute (MDPI) | ||||||||||||||||||||
| Name der Reihe: | Smart Structures and Systems: Actual Scientific and Industrial Research | ||||||||||||||||||||
| ISSN: | 2673-3161 | ||||||||||||||||||||
| Status: | veröffentlicht | ||||||||||||||||||||
| Stichwörter: | morphing compressor blades; aerostructural coupled design | ||||||||||||||||||||
| HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||||||||||||||
| HGF - Programm: | Luftfahrt | ||||||||||||||||||||
| HGF - Programmthema: | Umweltschonender Antrieb | ||||||||||||||||||||
| DLR - Schwerpunkt: | Luftfahrt | ||||||||||||||||||||
| DLR - Forschungsgebiet: | L CP - Umweltschonender Antrieb | ||||||||||||||||||||
| DLR - Teilgebiet (Projekt, Vorhaben): | L - Triebwerkskonzepte und -integration, L - keine Zuordnung, L - Wirkung | ||||||||||||||||||||
| Standort: | Braunschweig | ||||||||||||||||||||
| Institute & Einrichtungen: | Institut für Faserverbundleichtbau und Adaptronik > Adaptronik | ||||||||||||||||||||
| Hinterlegt von: | Montano Rejas, Zhuzhell | ||||||||||||||||||||
| Hinterlegt am: | 20 Apr 2022 09:37 | ||||||||||||||||||||
| Letzte Änderung: | 11 Jan 2023 15:01 |
Verfügbare Versionen dieses Eintrags
- A Coupling Method for the Design of Shape-Adaptive Compressor Blades. (deposited 20 Apr 2022 09:37) [Gegenwärtig angezeigt]
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