In this work, a simple methodology for preliminarily assessing the magnitude of potential landslide-induced impulse waves’ attenuation in mountain lakes is presented. A set of metrics is used to define the geometries of theoretical mountain lakes of different sizes and shapes and to simulate impulse waves in them using the hydrodynamic software Flow-3D. The modeling results provide the ‘wave decay potential’, a ratio between the maximum wave amplitude and the flow depth at the shoreline. Wave decay potential is highly correlated with what is defined as the ‘shape product’, a metric that represents lake geometry. The relation between these two parameters can be used to evaluate wave dissipation in a natural lake given its geometric properties, and thus estimate expected flow depth at the shoreline. This novel approach is tested by applying it to a real-world event, the 2007 landslide-generated wave in Chehalis Lake (Canada), where the results match well with those obtained using the empirical equation provided by ETH Zurich (2019 Edition). This work represents the initial stage in the development of this method, and it encourages additional research and modeling in which the influence of the impacting characteristics on the resulting waves and flow depths is investigated.
Abstract. This study aims to test the capacity of Flow-3D regarding the simulation of a rockslide-generated impulse wave by evaluating the influences of the extent of the computational domain, the grid resolution, and the corresponding computation times on the accuracy of modelling results. A detailed analysis of the Lituya Bay tsunami event (1958, Alaska, maximum recorded run-up of 524 m a.s.l.) is presented. A focus is put on the tsunami formation and run-up in the impact area. Several simulations with a simplified bay geometry are performed in order to test the concept of a “denser fluid”, compared to the seawater in the bay, for the impacting rockslide material. Further, topographic and bathymetric surfaces of the impact area are set up. The observed maximum run-up can be reproduced using a uniform grid resolution of 5 m, where the wave overtops the hill crest facing the slide source and then flows diagonally down the slope. The model is extended along the entire bay to simulate the wave propagation. The tsunami trimline is well recreated when using (a) a uniform mesh size of 20 m or (b) a non-uniform mesh size of 15 m × 15 m × 10 m with a relative roughness of 2 m for the topographic surface. The trimline mainly results from the primary wave, and in some locations it also results from reflected waves. The denser fluid is a suitable and simple concept to recreate a sliding mass impacting a waterbody, in this case with maximum impact speed of ∼93 m s−1. The tsunami event and the related trimline are well reproduced using the 3D modelling approach with the density evaluation model available in Flow-3D.
The recent demand for sustainable aviation designs challenges aircraft manufacturers to reconsider existing technologies in light of the required cuts in environmental pollution. One of the key factors in addressing these green targets is represented by the integration of unconventional propulsion concepts on the airframe, exploiting electrically driven designs. Among the necessary targets to achieve, a substantial noise emission reduction is needed. Since the new aircraft designs could include existing or novel propulsion system components to address the challenge of reliably predicting noise emissions, in this work a simplified, fast and physicalprinciples-based rotor noise model is introduced, together with suitable adapted perturbation equations to represent current and possibly newly arising noise sources mechanisms. The rotor noise model is based on rotating point or line sources that represent loading noise in terms of equivalent body forces. The model is applied in a Computational Aeroacoustics (CAA) framework in the time domain. The Linearized Euler Equations (LEE) are split into two separate perturbation equation systems for the acoustic and vorticity mode, respectively. The new noise prediction model, together with the new equations, are implemented in the unstructured quadrature-free experimental Discontinuous Galerkin (DG) CAA solver DISCO++ of DLR. Acoustic Perturbation Equations (APE) describe the propagation of the acoustic mode, and can be discretized numerically very robustly in the DG-framework. The equation splitup intends to overcome numerical stability issues present in the discretization of the LEE with the DG method. The paper reports initial successful results and outlines future possible applications.
On 17 October 2015, a large-scale subaerial landslide occurred in Taan Fiord, Alaska, which released about 50 Mm3 of rock. This entered the water body and triggered a tsunami with a runup of up to 193 m. This paper aims to simulate the possible formation of a weak layer in this mountainous slope until collapse, and to analyze the possible triggering factors of this landslide event from a geotechnical engineering perspective so that a deeper understanding of this large landslide event can be gained. We analyzed different remote-sensing datasets to characterize the evolution of the coastal landslide process. Based on the acquired remote-sensing data, Digital Elevation Models were derived, on which we employed a 2D limit equilibrium method in this study to calculate the safety factor and compare the location of the associated sliding surface with the most probable actual location at which this landslide occurred. The calculation results reflect the development process of this slope collapse. In this case study, past earthquakes, rainfall before this landslide event, and glacial melting at the toe may have influenced the stability of this slope. The glacial retreat is likely to be the most significant direct triggering factor for this slope failure. This research work illustrates the applicability of multi-temporal remote sensing data of slope morphology to constrain preliminary slope stability analyses, aiming to investigate large-scale landslide processes. This interdisciplinary approach confirms the effectiveness of the combination of aerial data acquisition and traditional slope stability analyses. This case study also demonstrates the significance of a climate change for landslide hazard assessment, and that the interaction of natural hazards in terms of multi-hazards cannot be ignored.
The increasing demand for cuts in environmental pollution is driving aircraft manufacturers towards sustainable aviation concepts that integrate unconventional propulsion configurations on the airframe. To aid the design process of new aircraft, a reliable prediction of installed rotor noise emissions would be required. Therefore, in this work an advanced rotor noise prediction approach is presented, which was developed to be fast and physical-principles-based, in order to be able to represent current and possibly newly arising noise sources mechanisms in complex configurations. The tool-chain proposed relies on aerodynamic predictions based on Actuator Disc (AD) Reynolds Averaged Navier Stokes (RANS) computations that provide the background flow solution for the Computational Aeroacoustics (CAA) method, which considers Gaussian regularised line-source distributions of strengths defined from either the obtained AD surface loads solution, or tabulated aerodynamic data used in combination with a model based on Blade Element Momentum Theory (BEMT). In this work initial successful results are reported for simplified test cases, outlining future possible applications.
A turbulent convective flow of an incompressible fluid inside a staggered ribbed channel with high blockage at ReH ≈ 4200 is simulated with direct numerical simulation (DNS) and Reynolds-averaged Navier–Stokes (RANS) techniques. The DNS results provide the reference solution for comparison of the RANS turbulence models. The k–ε realizable, k–ω SST, and v2¯–f model are accurately analyzed for their strengths and weaknesses in predicting the flow and temperature field for this geometry. These three models have been extensively used in literature to simulate this configuration and boundary conditions but with discordant conclusions upon their performance. The v2¯–f model performs much better than the k–ε realizable while the k–ω SST model results to be inadequate.
scite is a Brooklyn-based organization that helps researchers better discover and understand research articles through Smart Citations–citations that display the context of the citation and describe whether the article provides supporting or contrasting evidence. scite is used by students and researchers from around the world and is funded in part by the National Science Foundation and the National Institute on Drug Abuse of the National Institutes of Health.
hi@scite.ai
10624 S. Eastern Ave., Ste. A-614
Henderson, NV 89052, USA
Copyright © 2024 scite LLC. All rights reserved.
Made with 💙 for researchers
Part of the Research Solutions Family.