TY - THES A1 - Kavrakov, Igor T1 - Synergistic Framework for Analysis and Model Assessment in Bridge Aerodynamics and Aeroelasticity N2 - Wind-induced vibrations often represent a major design criterion for long-span bridges. This work deals with the assessment and development of models for aerodynamic and aeroelastic analyses of long-span bridges. Computational Fluid Dynamics (CFD) and semi-analytical aerodynamic models are employed to compute the bridge response due to both turbulent and laminar free-stream. For the assessment of these models, a comparative methodology is developed that consists of two steps, a qualitative and a quantitative one. The first, qualitative, step involves an extension of an existing approach based on Category Theory and its application to the field of bridge aerodynamics. Initially, the approach is extended to consider model comparability and completeness. Then, the complexity of the CFD and twelve semi-analytical models are evaluated based on their mathematical constructions, yielding a diagrammatic representation of model quality. In the second, quantitative, step of the comparative methodology, the discrepancy of a system response quantity for time-dependent aerodynamic models is quantified using comparison metrics for time-histories. Nine metrics are established on a uniform basis to quantify the discrepancies in local and global signal features that are of interest in bridge aerodynamics. These signal features involve quantities such as phase, time-varying frequency and magnitude content, probability density, non-stationarity, and nonlinearity. The two-dimensional (2D) Vortex Particle Method is used for the discretization of the Navier-Stokes equations including a Pseudo-three dimensional (Pseudo-3D) extension within an existing CFD solver. The Pseudo-3D Vortex Method considers the 3D structural behavior for aeroelastic analyses by positioning 2D fluid strips along a line-like structure. A novel turbulent Pseudo-3D Vortex Method is developed by combining the laminar Pseudo-3D VPM and a previously developed 2D method for the generation of free-stream turbulence. Using analytical derivations, it is shown that the fluid velocity correlation is maintained between the CFD strips. Furthermore, a new method is presented for the determination of the complex aerodynamic admittance under deterministic sinusoidal gusts using the Vortex Particle Method. The sinusoidal gusts are simulated by modeling the wakes of flapping airfoils in the CFD domain with inflow vortex particles. Positioning a section downstream yields sinusoidal forces that are used for determining all six components of the complex aerodynamic admittance. A closed-form analytical relation is derived, based on an existing analytical model. With this relation, the inflow particles’ strength can be related with the target gust amplitudes a priori. The developed methodologies are combined in a synergistic framework, which is applied to both fundamental examples and practical case studies. Where possible, the results are verified and validated. The outcome of this work is intended to shed some light on the complex wind–bridge interaction and suggest appropriate modeling strategies for an enhanced design. T3 - Schriftenreihe des DFG Graduiertenkollegs 1462 Modellqualitäten // Graduiertenkolleg Modellqualitäten - 21 KW - Brücke KW - Bridge KW - Computational Fluid Dynamics KW - Aerodynamics KW - Aeroelasticity KW - Category Theory KW - Aerodynamik KW - Aeroelastizität Y1 - 2020 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:gbv:wim2-20200316-41099 UR - https://asw-verlage.de/katalog/?id=2255 SN - 978-3-95773-284-2 PB - Bauhaus-Universitätsverlag CY - Weimar ER - TY - THES A1 - Abbas, Tajammal T1 - Assessment of Numerical Prediction Models for Aeroelastic Instabilities of Bridges N2 - The phenomenon of aerodynamic instability caused by the wind is usually a major design criterion for long-span cable-supported bridges. If the wind speed exceeds the critical flutter speed of the bridge, this constitutes an Ultimate Limit State. The prediction of the flutter boundary, therefore, requires accurate and robust models. The complexity and uncertainty of models for such engineering problems demand strategies for model assessment. This study is an attempt to use the concepts of sensitivity and uncertainty analyses to assess the aeroelastic instability prediction models for long-span bridges. The state-of-the-art theory concerning the determination of the flutter stability limit is presented. Since flutter is a coupling of aerodynamic forcing with a structural dynamics problem, different types and classes of structural and aerodynamic models can be combined to study the interaction. Here, both numerical approaches and analytical models are utilised and coupled in different ways to assess the prediction quality of the coupled model. T3 - Schriftenreihe des DFG Graduiertenkollegs 1462 Modellqualitäten // Graduiertenkolleg Modellqualitäten - 16 KW - Brücke KW - Flattern KW - Unsicherheit KW - Flutter KW - Bridges KW - Sensitivity KW - Uncertainty KW - Model assessment Y1 - 2016 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:gbv:wim2-20180515-27161 UR - https://asw-verlage.de/katalog/assessment_of_numerical_prediction_models_for_aeroelastic_instabilities_of_bridges-1897.html PB - Jonas Verlag CY - Weimar ER - TY - THES A1 - Bayer, Veit T1 - Zur Zuverlässigkeitsbeurteilung von Baukonstruktionen unter dynamischen Einwirkungen T1 - On the reliability assessment of building structures subjected to dynamic excitation N2 - Die Arbeit befaßt sich mit varianzmindernden Verfahren zur Monte Carlo Simulation von stochastischen Prozessen, zum Zweck der Zuverlässigkeitsbeurteilung von Baukonstruktionen mit nichtlinearem Systemverhalten. Kap. 2 ist eine Literaturstudie zu varianzmindernden Monte Carlo Methoden. In Kap. 3 wird die Spektrale Darstellung eines stationären, skalaren Gauß - Prozesses hergeleitet. Auf dieser Grundlage werden verschiedene Simulationsmodelle diskutiert. Das in Kap. 4 entwickelte varianzmindernde Simulationsverfahren basiert auf der Spektralen Darstellung. Nach einer ersten Pilotsimulation werden die Frequenzen für die Einführung zufälliger Amplituden bestimmt und deren Parameter angepaßt. Der zweite Lauf erfolgt mit diesen Parametern nach dem Prinzip des Importance Sampling. Das Verfahren wird in Kap. 5 für eine Brücke unter Erdbebenbelastung angewendet. Die Brücke ist mit sog. Hysteretic Devices zur Energiedissipation ausgerüstet. Es werden einerseits die Genauigkeit und Effizienz des Simulationsverfahrens, andererseits die Leistungsfähigkeit der Hysteretic Devices zur Erdbebenertüchtigung von Bauwerken demonstriert. N2 - Main topic is the development of variance–reducing Monte Carlo methods, for the purpose of reliability analyses of engineering structures with nonlinear behaviour. Ch. 2 is a literature survey on variance-reducing Monte Carlo methods. The Spectral Representation of a scalar, stationary Gaussian process is derived in ch. 3. On this basis, two popular simulation methods are discussed. The variance-reducing simulation concept developed in ch. 4 is based on the Spectral Representation. After a first pilot simulation, the frequencies are selected for introduction of amplitudes as random variables. In addition, the parameters of the amplitudes are adapted. This is the basis for the second simulation following the Importance Sampling principle. This simulation concept is utilized for reliability analysis of a bridge subjected to earthquake excitation in ch. 5. The bridge is equipped with Hysteretic Devices for dissipation of energy. The example demonstrates, on one hand, the accuracy and efficiency of the developed simulation method. On the other hand, the effectiveness of Hysteretic Devices for earthquake protection of building structures becomes evident. KW - Baukonstruktion KW - Dynamische Belastung KW - Zuverlässigkeit KW - Sicherheitstheorie KW - Erdbeben KW - Probabilistik KW - Brücke KW - Monte-Carlo Simulation KW - reliability assessment KW - earthquake KW - probabilistics KW - bridge KW - Monte Carlo simulation Y1 - 1999 U6 - http://nbn-resolving.de/urn/resolver.pl?urn:nbn:de:gbv:wim2-20040205-215 ER -