Babij, Georg (2024) Comparison of a Strong and a Weak Coupling Scheme for Aeroelastic Computations of a Rotor with Double-Swept Blades. 24. DGLR STAB-Symposium 2024, 2024-11-13 - 2024-11-14, Regensburg, Deutschland.
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Kurzfassung
High-fidelity aeroelastic simulations of rotor systems are carried out by coupling solvers of computational fluid dynamics (CFD) and a multibody system (MBS) with each other, namely the DLR Tau-Code and Simpack. In order to achieve this, aerodynamic forces and structural displacements on the blades as well as rigid body motions are exchanged between both solvers. Considering a strong coupling scheme, data is exchanged after each physical time step which makes it suitable for the use in time-transient simulations. While seeking for a periodic steady-state, e.g. a helicopter in forward or hovering flight, the precise simulation of transients is of minor importance. With this in mind, the wall-clock time of the simulation chain can be minimized by reducing the overhead resulting from frequent data exchange and extensive switching between both solvers. The implemented method is characterized by a weak coupling scheme which denotes a data exchange of an entire rotor revolution. In addition, the coupling window is phase-shifted after each iteration step by choosing an additional phase added to the end of one rotor revolution. It is applied to a model rotor with double-swept blades. In the end, a comparison for the blade tip displacement was made with results from a strong coupling scheme showing different curves, mainly with regrad to the peak values in the transition phase from up- to downstroke.
elib-URL des Eintrags: | https://elib.dlr.de/208942/ | ||||||||
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Dokumentart: | Konferenzbeitrag (Vortrag) | ||||||||
Titel: | Comparison of a Strong and a Weak Coupling Scheme for Aeroelastic Computations of a Rotor with Double-Swept Blades | ||||||||
Autoren: |
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Datum: | 13 November 2024 | ||||||||
Referierte Publikation: | Ja | ||||||||
Open Access: | Nein | ||||||||
Gold Open Access: | Nein | ||||||||
In SCOPUS: | Nein | ||||||||
In ISI Web of Science: | Nein | ||||||||
Status: | veröffentlicht | ||||||||
Stichwörter: | Aeroelastic Coupling, Computational Fluid Dynamics, Multibody System, Rotor Aeroelasticity, Dynamic Stall | ||||||||
Veranstaltungstitel: | 24. DGLR STAB-Symposium 2024 | ||||||||
Veranstaltungsort: | Regensburg, Deutschland | ||||||||
Veranstaltungsart: | nationale Konferenz | ||||||||
Veranstaltungsbeginn: | 13 November 2024 | ||||||||
Veranstaltungsende: | 14 November 2024 | ||||||||
Veranstalter : | Deutsche Strömungsmechanische Arbeitsgemeinschaft (STAB) | ||||||||
HGF - Forschungsbereich: | Luftfahrt, Raumfahrt und Verkehr | ||||||||
HGF - Programm: | Luftfahrt | ||||||||
HGF - Programmthema: | Effizientes Luftfahrzeug | ||||||||
DLR - Schwerpunkt: | Luftfahrt | ||||||||
DLR - Forschungsgebiet: | L EV - Effizientes Luftfahrzeug | ||||||||
DLR - Teilgebiet (Projekt, Vorhaben): | L - Virtueller Hubschrauber und Validierung | ||||||||
Standort: | Göttingen | ||||||||
Institute & Einrichtungen: | Institut für Aeroelastik > Aeroelastische Simulation | ||||||||
Hinterlegt von: | Babij, Georg | ||||||||
Hinterlegt am: | 21 Nov 2024 10:01 | ||||||||
Letzte Änderung: | 21 Nov 2024 10:01 |
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