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COUPLED FLUID STRUCTURE SIMULATION METHOD IN THE FREQUENCY DOMAIN FOR TURBOMACHINERY APPLICATIONS

Berthold, Christian und Frey, Christian und Schönenborn, Harald (2018) COUPLED FLUID STRUCTURE SIMULATION METHOD IN THE FREQUENCY DOMAIN FOR TURBOMACHINERY APPLICATIONS. In: Proceedings of the ASME Turbo Expo. Proceedings of ASME Turbo Expo 2018, 2018-06-11 - 2018-06-15, Oslo. doi: 10.1115/GT2018-76220.

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Kurzfassung

Turbomachinery components are exposed to unsteady aero- dynamic loads which must be considered during the design pro- cess to ensure the structural mechanical integrity. There are two primary mechanisms which cause structural vibrations and can lead to high-cycle fatigue due to high dynamic stresses: flutter (self-excited vibrations) and forced response (forced excitation, e.g. wakes from upstream blade rows). In this work an emerging numerical frequency-domain method which is designed to effi- ciently simulate coupled fluid-structure interaction (FSI) prob- lems considering nonlinearities in the flow and structure is mod- ified and applied to an academic and a realistic test case. Fur- thermore complex structural eigenmodes are considered instead of purely real modes as was demonstrated in the literature so far. This method is able to predict limit cycle oscillations and forced response amplitudes. The coupled solver uses the Har- monic Balance (HB) method with an alternating frequency time approach to model periodically unsteady flows and structure dy- namics. The resulting nonlinear HB equations of the flow are solved with a pseudo-time stepping method while the nonlinear HB equations of the structure are solved with a Newton method. The dynamics of the involved structure are further simplified by considering only one relevant eigenmode of the structure. The method is applied to a 3D axial turbine configuration with a mod- ified Youngs modulus for the material of the blisk. The standard flutter curve of the blade row shows that at least one eigenmode is aerodynamically unstable at certain nodal diameters. As a first model test case for the harmonic balance solver, the non- linear structural damping is defined as a cubic modal damping term. The results of the frequency-domain method are compared to coupled FSI simulations in the time domain. The analysis shows that the frequency-domain method is very promising in terms of both computational efficiency and accuracy.

elib-URL des Eintrags:https://elib.dlr.de/120686/
Dokumentart:Konferenzbeitrag (Vortrag)
Titel:COUPLED FLUID STRUCTURE SIMULATION METHOD IN THE FREQUENCY DOMAIN FOR TURBOMACHINERY APPLICATIONS
Autoren:
AutorenInstitution oder E-Mail-AdresseAutoren-ORCID-iDORCID Put Code
Berthold, ChristianChristian.Berthold (at) dlr.deNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Frey, ChristianChristian.Frey (at) dlr.dehttps://orcid.org/0000-0003-0496-9225NICHT SPEZIFIZIERT
Schönenborn, HaraldMTU Aero Engines GmbHNICHT SPEZIFIZIERTNICHT SPEZIFIZIERT
Datum:2018
Erschienen in:Proceedings of the ASME Turbo Expo
Referierte Publikation:Ja
Open Access:Nein
Gold Open Access:Nein
In SCOPUS:Ja
In ISI Web of Science:Nein
DOI:10.1115/GT2018-76220
Name der Reihe:Turbomachinery Technical Conference and Exposition
Status:veröffentlicht
Stichwörter:FSI, Turbomachinery, Flutter, Harmonic Balance, Fluid Structure Interaction
Veranstaltungstitel:Proceedings of ASME Turbo Expo 2018
Veranstaltungsort:Oslo
Veranstaltungsart:internationale Konferenz
Veranstaltungsbeginn:11 Juni 2018
Veranstaltungsende:15 Juni 2018
Veranstalter :ASME
HGF - Forschungsbereich:Luftfahrt, Raumfahrt und Verkehr
HGF - Programm:Luftfahrt
HGF - Programmthema:keine Zuordnung
DLR - Schwerpunkt:Luftfahrt
DLR - Forschungsgebiet:L - keine Zuordnung
DLR - Teilgebiet (Projekt, Vorhaben):L - keine Zuordnung
Standort: Köln-Porz
Institute & Einrichtungen:Institut für Antriebstechnik > Numerische Methoden
Hinterlegt von: Berthold, Christian
Hinterlegt am:29 Jun 2018 09:04
Letzte Änderung:24 Apr 2024 20:24

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