Relevant bibliographies by topics / Overset mesh

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Book chapters
  4. Conference papers

Academic literature on the topic 'Overset mesh'

Author: Grafiati
Published: 4 June 2021
Last updated: 9 February 2022

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Journal articles on the topic "Overset mesh"

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Shibliyev, Orxan, and Ibrahim Sezai. "Overset Grid Assembler and Flow Solver with Adaptive Spatial Load Balancing." Applied Sciences 11, no. 11 (2021): 5132. http://dx.doi.org/10.3390/app11115132.

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An overset mesh approach is useful for unsteady flow problems which involve components moving relative to each other. Since the generation of a single mesh around all components is prone to mesh stretching due to the relative motion of bodies, using the overset grid methodology, an individual mesh can be generated for each component. In this study, a parallel overset grid assembler was developed to establish connectivity across component meshes. Connectivity information was transferred to the developed parallel flow solver. The assembler uses multiple methods such as alternating digital tree and stencil walking to reduce the time spent on domain connectivity. Both the assembler and solver were partitioned spatially so that overlapping mesh blocks reside in the same partitions. Spatial partitioning was performed using a 3D space partitioning structure, namely octree, to which mesh blocks are registered. The octree was refined adaptively until bins of octree could be evenly distributed to processors. The assembler and solver were tested on a generic helicopter configuration in terms of load balance, scalability, and memory usage.
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Abbruzzese, Gennaro, Mariola Gómez, and Marta Cordero-Gracia. "Unstructured 2D grid generation using overset-mesh cutting and single-mesh reconstruction." Aerospace Science and Technology 78 (July 2018): 637–47. http://dx.doi.org/10.1016/j.ast.2018.05.004.

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Ma, Wenpeng, Xiaodong Hu, and Xiazhen Liu. "Parallel multibody separation simulation using MPI and OpenMP with communication optimization." Journal of Algorithms & Computational Technology 13 (September 7, 2018): 174830181879706. http://dx.doi.org/10.1177/1748301818797062.

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In this paper we investigate parallel implementations of multibody separation simulation using a hybrid of message passing interface and OpenMP. We propose a mesh block-based overset communication optimization algorithm. After presenting details of local data structures, we present our strategy for parallelizing both the overset mesh assembler and the flow solver by employing message passing interface and OpenMP. Experimental results show that the mesh block-based overset communication optimization algorithm has an advantage in real elapsed time when compared to a process-based implementation. The hybrid version shows that it is suitable for improving the load balance if a large number of CPU cores are used. We report results for a standard multibody separation case.
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Hu, Li-fen, Hao Wu, Qingtao Gong, Xiangyang Wang, and Wenbin Lv. "Time-Domain Flooding Simulation of a Damaged Warship." Marine Technology Society Journal 54, no. 2 (2020): 69–78. http://dx.doi.org/10.4031/mtsj.54.2.7.

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AbstractUnderstanding of the complex dynamic behavior of damaged ships and floodwater remains limited for ship designers and safety authorities. In this work, a Navier-Stokes (NS) solver that combines the volume of fluid (VOF) method with overset mesh techniques is developed to simulate the flooding process of a damaged ship. The VOF method captures the fluid interface, and the turbulence effect on flows is considered with the k-ω model. The overset mesh techniques are employed to handle the mesh update following transient ship motions. Then, the results of a damaged barge with dynamic and overset mesh are compared with the experimental data. On the basis of this validation, the solver is applied to the flooding problems of a damaged warship. This research is intended to be a useful step toward the establishment of a stability criterion for damaged ships in the future.
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Jarkowski, M., M. A. Woodgate, G. N. Barakos, and J. Rokicki. "Towards consistent hybrid overset mesh methods for rotorcraft CFD." International Journal for Numerical Methods in Fluids 74, no. 8 (2013): 543–76. http://dx.doi.org/10.1002/fld.3861.

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Horne, Wyatt James, and Krishnan Mahesh. "A massively-parallel, unstructured overset method for mesh connectivity." Journal of Computational Physics 376 (January 2019): 585–96. http://dx.doi.org/10.1016/j.jcp.2018.09.053.

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Hall, David M., and Ramachandran D. Nair. "Discontinuous Galerkin Transport on the Spherical Yin–Yang Overset Mesh." Monthly Weather Review 141, no. 1 (2013): 264–82. http://dx.doi.org/10.1175/mwr-d-12-00108.1.

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Abstract A discontinuous Galerkin (DG) transport scheme is presented that employs the Yin–Yang grid on the sphere. The Yin–Yang grid is a quasi-uniform overset mesh comprising two notched latitude–longitude meshes placed at right angles to each other. Surface fluxes of conserved scalars are obtained at the overset boundaries by interpolation from the interior of the elements on the complimentary grid, using high-order polynomial interpolation intrinsic to the DG technique. A series of standard tests are applied to evaluate its performance, revealing it to be robust and its accuracy to be competitive with other global advection schemes at equivalent resolutions. Under p-type grid refinement, the DG Yin–Yang method exhibits spectral error convergence for smooth initial conditions and third-order geometric convergence for C1 continuous functions. In comparison with finite-volume implementations of the Yin–Yang mesh, the DG implementation is less complex, as it does not require a wide halo region of elements for accurate boundary value interpolation. With respect to DG cubed-sphere implementations, the Yin–Yang grid exhibits similar accuracy and appears to be a viable alternative suitable for global advective transport. A variant called the Yin–Yang polar (YY-P) mesh is also examined and is shown to have properties similar to the original Yin–Yang mesh while performing better on tests with strictly zonal flow.
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Fathuddiin, Abubakar, Samuel Samuel, Kiryanto Kiryanto, and Aulia Widyandari. "Prediksi Hambatan Kapal dengan Menggunakan Metode Overset Mesh pada Kapal Planing Hull." Jurnal Rekayasa Hijau 4, no. 1 (2020): 24–34. http://dx.doi.org/10.26760/jrh.v4i1.24-34.

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ABSTRAKPrediksi hambatan kapal tipe planing lebih rumit dibanding dengan tipe displacement, hal ini disebabkan oleh gaya hidrodinamis yang lebih dominan pada bagian bawah kapal. Karakteristik hambatan kapal tipe planing sangat dipengaruhi oleh gerakan trim dan heave. Selain itu, bentuk hullform juga mempengaruhi hambatan kapal; seperti sudut dead-rise, chine, strip, stephull, dan lain-lain. Solusi untuk memprediksi hambatan kapal dengan menggunakan Finite Volume Method (FVM). Persamaan RANS (Reynolds- Averaged Navier-Stokes) dengan model turbulensi k-ε untuk memprediksi aliran turbulen dan Volume of Fluid (VOF) untuk mempresentasikan aliran 2 fasa. Pada penelitian ini digunakan metode overset mesh untuk memprediksi hambatan kapal agar mendapatkan akurasi yang baik. Hasil simulasi hambatan menunjukkan trend yang baik. Pada kecepatan tinggi, prediksi hambatan tidak memiliki hasil yang baik. Solusi yang ditawarkan pada Numerical ventilation problem (NVP) adalah dengan menggunakan metode phase replacement.Kata kunci: CFD, planing hull, RANS, overset mesh, NVP ABSTRACTThe prediction of planing hull resistance is more complicated than the displacement hull. It is caused by the more dominant hydrodynamic force at the bottom of the ship. The planing hull resistance characteristics are strongly influenced by trim and heave movements. In addition, the shape of the hullform also affects the ship's resistance, such as dead-rise angle, chine, strip, stephull, and others. The solution to predict ship resistance is by using the Finite Volume Method (FVM). RANS (Reynolds-Averaged Navier-Stokes) equation k-ε turbulence model was used to predict turbulent flow and Volume of Fluid (VOF) to present 2 phase flow. In this study, the overset mesh method was used to predict ship resistance in order to get good accuracy. Resistance simulation results showed a good trend. At high speeds, the prediction of resistance did not have good results. The solution offered in the Numerical ventilation problem (NVP) was to use the phase replacement method.Keywords: CFD, planing hull, RANS, overset mesh, NVP
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Lee, Byung Joon, and Chongam Kim. "Aerodynamic Redesign Using Discrete Adjoint Approach on Overset Mesh System." Journal of Aircraft 45, no. 5 (2008): 1643–53. http://dx.doi.org/10.2514/1.34112.

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Shenoy, Rajiv, Marilyn J. Smith, and Michael A. Park. "Unstructured Overset Mesh Adaptation with Turbulence Modeling for Unsteady Aerodynamic Interactions." Journal of Aircraft 51, no. 1 (2014): 161–74. http://dx.doi.org/10.2514/1.c032195.

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Dissertations / Theses on the topic "Overset mesh"

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Lyons, David Geoffrey. "Implications of Shallow Water in Numerical Simulations of a Surface Effect Ship." Thesis, Virginia Tech, 2014. http://hdl.handle.net/10919/52558.

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Overset, or Chimera, meshes are used to discretize the governing equations within a computational domain using multiple meshes that overlap in an arbitrary manner. The overset meshing technique is most applicable to problems dealing with multiple or moving bodies. Deep water simulations were carried out using both single and overset grid techniques for the evaluation of the overset grid application. These simulations were carried out using the commercial CFD code STAR-CCM+ by CD-adapco. The geometry simulated is that of a SES model (T-Craft) tested at the Naval Surface Warfare Center Carderock Division. The craft is simulated with two degrees of freedom, allowing movement in heave and pitch in response to displacement of the free surface. Agreement between the single and overset grid techniques was deemed reasonable to extend to future shallow water cases. However, due to longer run times of the overset mesh, the traditional or single mesh technique should be employed whenever applicable. In order to extend existing full craft CFD simulations of a surface effect ship (SES) into shallow water and maneuvering cases, an overset mesh is needed. Simulations of the SES were performed and monitored at various depth Froude numbers resulting in subcritical, critical, and supercritical flow regimes. Resistance, pitch response, and free surface response of the SES were compared between the shallow water simulations. The SES produced wider wakes, perpendicular to the craft, at simulations closer to the critical flow regime. Critical flow occurs at a depth Froude number between 0.9 and 0.95. Progression of shallow water effects through the three flow regimes agrees well with shallow water theory.<br>Master of Science
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Peron, Stephanie. "Méthode d'assemblage de maillages recouvrants autour de géométries complexes pour des simulations en aérodynamique compressible." Thesis, Paris, ENSAM, 2014. http://www.theses.fr/2014ENAM0026/document.

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La simulation numérique des écoulements (CFD) est largement utilisée aujourd'hui dans l'industrie aéronautique, de l'avant-projet à la conception des appareils. En parallèle, la puissance des calculateurs s'est accrue, permettant d'effectuer des simulations résolvant les équations de Navier-Stokes moyennées (RANS) dans un délai de restitution acceptable du point de vue industriel. Cependant, les configurations simulées sont de plus en plus complexes géométriquement, rendant la réalisation du maillage très coûteuse en temps humain. Notre objectif est de proposer une méthode permettant de simplifier la génération de maillages autour de géométries complexes, en exploitant les avantages de la méthode Chimère, tout en levant les difficultés principales rencontrées par cette méthode dans le calcul des connectivités. Dans notre approche, le domaine de calcul est découpé en régions proches et en régions éloignées des corps. Des grilles curvilignes de faible extension décrivent les régions autour des corps. Le maillage de fond est défini par un ensemble de grilles cartésiennes superposées aux grilles de corps, qui sont engendrées et adaptées automatiquement selon les caractéristiques de l'écoulement. Afin de traiter des maillages recouvrants autour de géométries complexes sans surcoût humain, les différentes grilles sont regroupées par composant Chimère. Des relations d'assemblage sont alors définies entre composants, en s'inspirant de la Géométrie de Construction des Solides (CSG), où un solide peut être construit par opérations booléennes successives entre solides primitifs. Le calcul des connectivités Chimère est alors réalisé de manière simplifiée. Des simulations RANS sont effectuées autour d'un fuselage d'hélicoptère avec mât de soufflerie et autour d'une aile NACA0015 en incidence, afin de mettre en oeuvre la méthode<br>Computational fluid dynamics (CFD) is widely used today in aeronautics, while the computing power has increased, enabling to perform simulations solving Reynolds-averaged Navier-Stokes equations (RANS) within an acceptable time frame from the industrial point of view. However, the configurations are more and more geometrically complex, making the mesh generation step prohibitive. Our aim is here to propose a method enabling a simplification of the mesh generation over complex geometries, taking advantage of the Chimera method and overcoming the major difficulties arising when performing overset grid connectivity. In our approach, the computational domain is partitioned into near-body regions and off-body regions. Near-body regions are meshed by curvilinear grids of short extension describing the obstacles involved in the simulation. Off-body mesh is defined by a set of adaptive Cartesian grids, overlapping near-body grids. In order to consider overset grids over complex geometries with no additional cost, grids are gathered by Chimera component, and assembly relations are defined between them, inspired by Constructive Solid Geometry, where a solid can result from boolean operations between primitive solids. The overset grid connectivity is thus simplified. RANS simulations are performed over a helicopter fuselage with a strut, and over a NACA0015 wing
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De, La Peña-Cortes Jesus Ernesto. "Development of fluid-solid interaction (FSI)." Thesis, University of Manchester, 2018. https://www.research.manchester.ac.uk/portal/en/theses/development-of-fluidsolid-interaction-fsi(b22b29e2-0349-44a9-ab18-eeb0717d18c8).html.

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This work extends a previously developed finite-volume overset-grid fluid flow solver to enable the characterisation of rigid-body-fluid interaction problems. To this end, several essential components have been developed and blended together. The inherent time-dependent nature of fluid-solid interaction problems is captured through the laminar transient incompressible Navier-Stokes equations for the fluid, and the Euler-Newton equations for rigid-body motion. First and second order accurate time discretisation schemes have been implemented for the former, whereas second and third order accurate time discretisation schemes have been made available for the latter. Without doubt the main advantage the overset-grid method offers regarding moving entities is the avoidance of the time consuming grid regeneration step, and the resulting grid distortion that can often cause numerical stability problems in the solution of the flow equations. Instead, body movement is achieved by the relative motion of a body fitted grid over a suitable background mesh. In this case, the governing equations of fluid flow are formulated using a Lagrangian, Eulerian, or hybrid flow description via the Arbitrary Lagrangian-Eulerian method. This entails the need to guarantee that mesh motion shall not disturb the flow field. With this in mind, the space conservation law has been hard-coded. The compliance of the space conservation law has the added benefit of preventing spurious mass sources from appearing due to mesh deformation. In this work, two-way fluid-solid interaction problems are solved via a partitioned approach. Coupling is achieved by implementing a Picard iteration algorithm. This allows for flexible degree of coupling specificationby the user. Furthermore, if strong coupling is desired, three variants of interface under-relaxation can be chosen to mitigate stability issues and to accelerate convergence. These include fixed, or two variants of Aitken’s adaptive under-relaxation factors. The software also allows to solve for one-way fluid-solid interaction problems in which the motion of the solid is prescribed. Verification of the core individual components of the software is carried out through the powerful method of manufactured solutions (MMS). This purely mathematically based exercise provides a picture of the order of accuracy of the implementation, and serves as a filter for coding errors which can be virtually impossible to detect by other means. Three instances of one-way fluid-solid interaction cases are compared with simulation results either from the literature, or from the OpenFOAM package. These include: flow within a piston cylinder assembly, flow induced by two oscillating cylinders, and flow induced by two rectangular plates exhibiting general planar motion. Three cases pertaining to the class of two-way fluid-interaction problems are presented. The flow generated by the free fall of a cylinder under the action of gravity is computed with the aid of an intermediate ‘motion tracking’ grid. The solution is compared with the one obtained using a vorticity based particle solver for validation purposes. Transverse vortex induced vibrations (VIV) of a circular cylinder immersed in a fluid, and subject to a stream are compared with experimental data. Finally, the fluttering motion of a rectangular plate under different scenarios is analysed.
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Kokkonen, Toni. "CFD analysis of stepped planing vessels." Thesis, KTH, Mekanik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-250023.

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High speed planing hulls are currently widely used for example in recreational and emergency vessel applications. However, very little CFD research has been done for planing vessels, especially for those with stepped hulls. A validated CFD method for planing stepped hulls could be a valuable improvement for the design phase of such hulls. In this thesis, a CFD method for stepped hulls, with a primary focus on two-step hulls, is developed using STAR-CCM+. As a secondary objective, porpoising instability of two-step hulls is investigated. The simulations are divided into two parts: In the first part a method is developed and validated with existing experimental and numerical data for a simple model scale planing hull with one step. In the second part the method is applied for two two-step hulls provided with Hydrolift AS. A maximum two degrees of freedom, trim and heave, are used, as well as RANS based k-w SST turbulence model and Volume of Fluid (VOF) as a free surface model. The results for the one-step hull mostly corresponded well with the validation data. For the two-step hulls, validation data did not exists and they were first simulated with a fixed trim and sinkage and compered between each other. In the simulations with free trim and heave both hulls experienced unstable porpoising behavior.
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Korfmann, Sören. "Simulative Bestimmung charakteristischer Rotorparameter von Multikoptern und Vergleich mit Versuchsergebnissen." 2020. https://tud.qucosa.de/id/qucosa%3A73678.

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Das Ziel dieser Forschungsarbeit ist die Bestimmung charakteristischer aerodynamischer Koeffizienten im Schwebeflug mit Hilfe von Strömungssimulationen. Diese Koeffizienten werden für eine modellbasierte Regelung eines vollaktuierten Multikopters benötigt. Für die Simulationen wird aufbauend auf vorangegangenen Arbeiten ein ‚Sliding-mesh‘-Modell optimiert und einem ‚Overset-mesh‘-Modell gegenübergestellt. Die Verfahren werden anhand von Mess- sowie Referenzdaten hinsichtlich ihrer Rechenzeit und Genauigkeit verglichen. Die Messdaten werden im Rahmen dieser Arbeit ausgewertet. Die Referenzdaten stammen aus älteren Untersuchungen. Das ‚Overset-mesh‘-Verfahren liefert bei viermal höherer Rechenzeit gleichwertige adäquate Ergebnisse. Aus diesen Gründen werden anknüpfende Untersuchungen des Zeitverhaltens der Rotorschubkraft bei Drehzahländerungen mit dem ‚Sliding-mesh‘-Modell durchgeführt. Es wird beobachtet, dass die Schubkraft innerhalb der Simulation den Messdaten bei Drehzahlsprüngen vorauseilt.:1 Einleitung 1.1 Motivation 1.2 Zielsetzung und Aufbau der Arbeit 2 Theoretische Grundlagen 2.1 Strömungsmechanik 2.1.1 Grundgleichungen 2.1.2 Zusätzliche Gleichungen 2.1.3 Navier-Stokes-Gleichungen 2.1.4 Laminare und turbulente Strömungen 2.1.5 Grenzschicht 2.2 Numerische Strömungsmechanik 2.2.1 Numerische Diskretisierung 2.2.2 Numerische Lösungsmodelle 2.2.3 Turbulenzmodelle 2.3 Rotorströmungen 2.3.1 Strahltheorie 2.3.2 Numerische Rotorsimulation 3 Stand der Technik 3.1 Motivation 3.2 Rotorströmung 3.3 Aeroelastizität 3.4 Nachlaufströmung 4 Umsetzung 4.1 Modellbildung 4.1.1 ‚Sliding-mesh‘-Verfahren 4.1.2 ‚Overset-mesh‘-Verfahren 4.2 Validierung 4.2.1 ‚Sliding-mesh‘-Verfahren 4.2.2 ‚Overset-mesh‘-Verfahren 4.3 Modifikationen 4.3.1 ‚Sliding-mesh‘-Verfahren 4.3.2 ‚Overset-mesh‘-Verfahren 4.4 Auswertung 4.4.1 ‚Sliding-mesh‘-Verfahren 4.4.2 ‚Overset-mesh‘-Verfahren 5 Messaufbau und Messauswertung 5.1 Messaufbau 5.2 Messauswertung 5.2.1 Schubkraftverlauf 5.2.2 Drehmomentenverlauf 6 Zeitverhalten 6.1 Modellbildung 6.2 Auswertung Schubkraftverlauf 6.2.1 Drehzahlsprung 1 6.2.2 Drehzahlsprung 2 7 Zusammenfassung und Ausblick 7.1 Zusammenfassung 7.2 Ausblick
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Book chapters on the topic "Overset mesh"

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Jung, Mun Seung, and Oh Joon Kwon. "Development of a Conservative Overset Mesh Method on Unstructured Meshes." In Computational Fluid Dynamics 2010. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-17884-9_118.

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Jung, Mun Seung, and Oh Joon Kwon. "A Parallel Unstructured Overset Mesh Technique for Unsteady Flow Simulations." In Computational Fluid Dynamics 2006. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-92779-2_48.

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Limare, Alexandre, Houman Borouchaki, and Pierre Brenner. "Adaptive Mesh Refinement with an Automatic Hybrid RANS/LES Strategy and Overset Grids." In Progress in Hybrid RANS-LES Modelling. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-27607-2_12.

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Mbandi, Josephine, and Michael Kisangari. "Data Collection Using Wireless Sensor Networks and Online Visualization for Kitui, Kenya." In African Handbook of Climate Change Adaptation. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-45106-6_151.

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AbstractKenya is a developing country with a population of 47,213,282 people this comprises of 56% low-income earners. Small businesses and crop production represent 23% of the income within the country, which is at risk as soils become less productive. Various factors have led to this, climate change and land overuse being leading causes. Without adaptation, the rural to urban migration will continue to increase.Through Internet of Things (IoT) and specifically wireless sensor networks, we can change how we obtain and consume information. Small-scale farmers can collect data and in exchange receive useful information about their soils, temperature, humidity, and moisture content hence make better choices during crop production. Connected end devices bring in data, which is currently sparse in relation to small-scale farming. IoT will enable analysis and informed decision-making including crop selection, support equipment, fertilizers, irrigation, and harvesting. The cloud-based analysis will provide information useful for policy making and improvement.This chapter presents a wireless sensor network (WSN) in mesh topography using XBee communication module, communication, and raspberry pi, combined with a cloud-based data storage and analysis. We successfully set up a proof of concept to test a sensor node that sends information to a RPi and onto an online visualization platform.
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Conference papers on the topic "Overset mesh"

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Clark, Colton G., David G. Lyons, and Wayne L. Neu. "Comparison of Single and Overset Grid Techniques for CFD Simulations of a Surface Effect Ship." In ASME 2014 33rd International Conference on Ocean, Offshore and Arctic Engineering. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/omae2014-24207.

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Overset, or Chimera meshes are used to discretize the governing equations within a computational domain using multiple meshes that overlap in an arbitrary manner. The overset mesh technique is most applicable to problems dealing with multiple or moving bodies. In order to extend existing full craft CFD (RANS) simulations of a surface effect ship (SES) into shallow water and maneuvering cases, an overset mesh is needed. Deep water simulations were carried out using both single and overset grid techniques for evaluation of the overset grid application. The single grid technique applies a hexahedral mesh to the fluid domain and SES geometry. An adequate mesh resolution was determined by performing a grid convergence study on a series of systematically refined meshes. An overset mesh of the same resolution was then constructed and was fixed to the body. Drag and pitch results are compared among the two simulations. Free surface elevations around the craft and under the air cushion for simulations with the single and overset meshes are compared. Steady-state simulations using the overset mesh and the single mesh show general similarities in drag, pitch, and free surface elevations.
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Khaware, Alok, Vinay Kumar Gupta, and Abhilash Rajan. "Numerical Simulation of Aerospace Applications Using Overset Mesh." In 2017 IEEE 24th International Conference on High Performance Computing Workshops (HiPCW). IEEE, 2017. http://dx.doi.org/10.1109/hipcw.2017.00018.

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Khaware, Alok, Vinay Kumar Gupta, KVSS Srikanth, and Mohammed Azhar. "Numerical Simulation of Cavitating Flows using Overset Mesh." In The 4th World Congress on Momentum, Heat and Mass Transfer. Avestia Publishing, 2019. http://dx.doi.org/10.11159/icmfht19.108.

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Khaware, Alok, Kvss Srikanth, and Vinay Kumar Gupta. "Numerical Simulation of Free Surface Flows Using Overset Mesh." In Offshore Technology Conference Asia. Offshore Technology Conference, 2018. http://dx.doi.org/10.4043/28461-ms.

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Pandya, Shishir, William Chan, and James Kless. "Automation of Structured Overset Mesh Generation for Rocket Geometries." In 19th AIAA Computational Fluid Dynamics. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-3993.

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Patel, Himanshu, and Martin Anto. "Oil Splash Simulation in Final Drive with Overset Mesh." In Symposium on International Automotive Technology 2019. SAE International, 2019. http://dx.doi.org/10.4271/2019-26-0274.

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Nastase, Cristian, Dimitri Mavriplis, and Jay Sitaraman. "An Overset Unstructured Mesh Discontinuous Galerkin Approach for Aerodynamic Problems." In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-195.

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Chan, William M., Shishir A. Pandya, and Robert Haimes. "Automation of Overset Structured Surface Mesh Generation on Complex Geometries." In AIAA Aviation 2019 Forum. American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-3671.

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Al-Azawy, Mohammed G., A. Turan, and A. Revell. "An Overset Mesh Approach for Valve Closure: An LVAD Application." In 9th International Conference on Biomedical Electronics and Devices. SCITEPRESS - Science and and Technology Publications, 2016. http://dx.doi.org/10.5220/0005663901450151.

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Tramel, Robert, Robert Nichols, Robert Tramel, and Robert Nichols. "A highly efficient numerical method for overset-mesh moving-body problems." In 13th Computational Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-2040.

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