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Comparison of a Strong and a Weak Coupling Scheme for Aeroelastic Computations of a Rotor with Double-Swept Blades

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/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:Comparison of a Strong and a Weak Coupling Scheme for Aeroelastic Computations of a Rotor with Double-Swept Blades
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Babij, GeorgGeorg.Babij (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
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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