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Projekt Druckansicht

Modellierung wirbelerregter aeroelastischer Schwingungen für Ermüdungsnachweise bei schlanken Baustrukturen

Antragstellerin Dr.-Ing. Francesca Lupi
Fachliche Zuordnung Angewandte Mechanik, Statik und Dynamik
Förderung Förderung von 2019 bis 2022
Projektkennung Deutsche Forschungsgemeinschaft (DFG) - Projektnummer 426322127
 
Erstellungsjahr 2023

Zusammenfassung der Projektergebnisse

Negative aerodynamic damping is the governing parameter for the onset of vortex-induced vibration (VIV). The first objective of the project was to investigate the negative aerodynamic damping of vortex induced vibrations using wind tunnel tests. These were carried out in the WISt boundary layer wind tunnel at the Ruhr-Universität Bochum. Different and complementary experimental approaches - forced vibration measurements on a sectional model, free vibration measurements on a sectional model and aeroelastic vibration of a cantilevered cylinder - are compared. None of these methods alone is sufficient to fully capture all aspects of the aeroelastic interaction in VIV, but their combination provides a clear insight into the phenomenon. The aim of this project is to calculate the response to vortex excitation using random vibration theory, which requires an equivalent linear aerodynamic damping model. The approach is consistent with forced vibration experimental results as negative aerodynamic damping is measured as a function of the root mean square of the vibration. In this way, forced vibration testing can be considered as a linearised stepwise testing technique for VIV. The response of slender structures to vortex excitation has a typical intermittent (or quasi-periodic) character due to a beat effect between the natural frequency of the structure and the vortex shedding frequency. Fatigue life is calculated using rainflow counting. Equivalent stresses can be derived that produce the same cumulative damage as the actual time histories with varying amplitude. VIV occurs not only when towers stand alone, but also when they are grouped together. In this case, depending on the relative distance between the cylinders, vortex streets develop not only behind the individual towers, but also behind the group as a whole. This interference further amplifies the vibration, particularly due to the gap flow that develops between the towers. For these reasons, specific criteria based on the experimental determination of allowable vibrations due to VIV in the presence of interference galloping are addressed. The most tangible success of this research project is the application of the concept developed for VIV to real structures. For example, the model is used to estimate the response of one of the world's largest and most powerful wind turbines, which in turn serves to validate the developed model. This validation is the subject of a subsequent DFG-funded Knowledge Transfer Project (Modellierung wirbelerregter aeroelastischer Schwingungen bei schlanken Baustrukturen: Erkenntnistransfer anhand eines großskaligen Feldversuchs an einer Windkraftanlage).

Projektbezogene Publikationen (Auswahl)

 
 

Zusatzinformationen

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