Готові списки джерел за темами / FLUENT SOLVER

Добірка наукової літератури з теми "FLUENT SOLVER"

Автор: Grafiati
Опубліковано: 11 вересня 2023

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Статті в журналах з теми "FLUENT SOLVER"

1

Pawłucki, Mateusz. "Multiple objective shape optimization in Ansys Fluent Solver." Mechanik, no. 11 (November 2015): 893–95. http://dx.doi.org/10.17814/mechanik.2015.11.587.

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2

Thwe, Kay, and Gao Gao. "An Evaluation of Model Ship Total Resistance by Measured and Different Methods." Applied Mechanics and Materials 110-116 (October 2011): 4433–38. http://dx.doi.org/10.4028/www.scientific.net/amm.110-116.4433.

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Анотація:
Prediction of total hull resistance has been investigated for many decades and it is still a challenging problem for naval architect. In this paper, the total resistance of round bilge monohull Model 100A is predicted by potential flow solver, Shipflow by Flowtech International AB, the commercial Reynold Average Navier Stroke (RANS) solver Fluent by Fluent, Inc., and analytical prediction by Slender Body Method (SBM). The total resistance was predicted by each code for the different model speeds (0.6m/s to 4.5m/s) and compared with experimental test data. The Fluent predictions were found to be in agreement with the experimental data in lower speed (0.6m/s to 2.5m/s). Shipflow results were more closed to experimental results than Fluent. Comparisons between the different solution methods were also discussed with the particular grid generation methods and numerical solution techniques. It is found that Slender Body Method can solve as easy and simple and it is effective to predict total resistance of thin ship monohull.
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3

Guo, Hao, Yimei Tian, Hailiang Shen, Yi Wang, and Mengxin Kang. "A landscape lake flow pattern design approach based on automated CFD simulation and parallel multiple objective optimization." Water Science and Technology 74, no. 5 (June 21, 2016): 1155–62. http://dx.doi.org/10.2166/wst.2016.308.

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Анотація:
A design approach for determining the optimal flow pattern in a landscape lake is proposed based on FLUENT simulation, multiple objective optimization, and parallel computing. This paper formulates the design into a multi-objective optimization problem, with lake circulation effects and operation cost as two objectives, and solves the optimization problem with non-dominated sorting genetic algorithm II. The lake flow pattern is modelled in FLUENT. The parallelization aims at multiple FLUENT instance runs, which is different from the FLUENT internal parallel solver. This approach: (1) proposes lake flow pattern metrics, i.e. weighted average water flow velocity, water volume percentage of low flow velocity, and variance of flow velocity, (2) defines user defined functions for boundary setting, objective and constraints calculation, and (3) parallels the execution of multiple FLUENT instances runs to significantly reduce the optimization wall-clock time. The proposed approach is demonstrated through a case study for Meijiang Lake in Tianjin, China.
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4

Aziz, M. S. Abdul, M. Z. Abdullah, C. Y. Khor, Z. M. Fairuz, A. M. Iqbal, M. Mazlan, and Mohd Sukhairi Mat Rasat. "Thermal Fluid-Structure Interaction in the Effects of Pin-Through-Hole Diameter during Wave Soldering." Advances in Mechanical Engineering 6 (January 1, 2014): 275735. http://dx.doi.org/10.1155/2014/275735.

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Анотація:
An effective simulation approach is introduced in this paper to study the thermal fluid-structure interaction (thermal FSI) on the effect of pin-through-hole (PTH) diameter on the wave soldering zone. A 3D single PTH connector and a printed circuit board model were constructed to investigate the capillary flow behavior when passing through molten solder (63SnPb37). In the analysis, the fluid solver FLUENT was used to solve and track the molten solder advancement using the volume of fluid technique. The structural solver ABAQUS was used to examine the von Mises stress and displacement of the PTH connector in the wave soldering process. Both solvers were coupled by MpCCI software. The effects of six different diameter ratios (0.1 < d/ D < 0.97) were studied through a simulation modeling. The use of ratio d/ D = 0.2 yielded a balanced filling profile and low thermal stress. Results revealed that filling level, temperature, and displacement exhibited polynomial behavior to d/ D. Stress of pin varied quadratically with the d/ D. The predicted molten solder profile was validated by experimental results. The simulation results are expected to provide better visualization and understanding of the wave soldering process by considering the aspects of thermal FSI.
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5

Kabdylkakov, Ye A., A. S. Suraev, and R. A. Irkimbekov. "APPLICATION OF THE TEXT INTERFACE OF THE ANSYS FLUENT PROGRAM FOR SIMULATION OF THE THERMOPHYSICAL STATE OF A TYPICAL EXPERIMENTAL DEVICE." NNC RK Bulletin, no. 3 (September 28, 2022): 55–63. http://dx.doi.org/10.52676/1729-7885-2022-3-55-63.

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Анотація:
The paper is dedicated to development of log of the ANSYS FLUENT program text commands. Although this program has well-developed and easy-to use graphical interface, command logs allow to conduct the configurations of the solver, optimizing the process of calculation justification safety of reactor experiments conducted at the “Institute of Atomic Energy” Branch of the RSE “National Nuclear Center of the Republic of Kazakhstan” (IAE Branch RSE NNC RK). Command logs allows to control the command to save the ANSYS FLUENT program solver as code in a separate file, which can later be used for other calculations. Command log allows to save settings the ANSYS FLUENT program solver as program code in a separate file, which can later be redacted and used for other calculations. Also, this would enable improving the group work of employees above one project, facilitate the exchange process of solver parameters and promptly make amendments and corrections. In the framework of this work, a technique for constructing a command log was developed for modeling thermophysical state of experimental devices in reactor experiments. The developed technique was tested on the example of solving a thermophysical task with a typical ED.
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6

Pajcin, Miroslav, Aleksandar Simonovic, Toni Ivanov, Dragan Komarov, and Slobodan Stupar. "Numerical analysis of a hypersonic turbulent and laminar flow using a commercial CFD solver." Thermal Science 21, suppl. 3 (2017): 795–807. http://dx.doi.org/10.2298/tsci160518198p.

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Анотація:
Computational fluid dynamics computations for two hypersonic flow cases using the commercial ANSYS FLUENT 16.2 CFD software were done. In this paper, an internal and external hypersonic flow cases were considered and analysis of the hypersonic flow using different turbulence viscosity models available in ANSYS FLUENT 16.2 as well as the laminar viscosity model were done. The obtained results were after compared and commented upon.
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7

Abdul Aziz, M. S., M. Z. Abdullah, and Kamarul Arifin Ahmad. "Numerical Investigations of Membrane Surface Effects on NACA 643- 218 Airfoil." Applied Mechanics and Materials 564 (June 2014): 60–65. http://dx.doi.org/10.4028/www.scientific.net/amm.564.60.

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Анотація:
This paper presents two dimensional fluid structure interaction (FSI) CFD analysis on the effect of skin thickness and Reynolds number on the aerodynamic performance of NACA 643-218 airfoil. Numerical investigations were performed using FLUENT 6.3 fluid flow solver and ABAQUS 6.8-1 structural solver. Coupling of both solvers in real time mode was accomplished with the Mesh based parallel Code Coupling Interface (MpCCI 3.1). The predicted and experimental results were found to be in excellent match. Generally, the results showed that the aerodynamic lift increases while drag decreases with the decrease of membrane thickness.
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8

Crha, Jakub, Pavlína Basařová, Marek C. Ruzicka, Ondřej Kašpar, and Maria Zednikova. "Comparison of Two Solvers for Simulation of Single Bubble Rising Dynamics: COMSOL vs. Fluent." Minerals 11, no. 5 (April 25, 2021): 452. http://dx.doi.org/10.3390/min11050452.

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Анотація:
Multiphase flows are a part of many industrial processes, where the bubble motion influences the hydrodynamic behavior of the batch. The current trend is to use numerical solvers that can simulate the movement and mutual interactions of bubbles. The aim of this work was to study how two commercial CFD solvers, COMSOL Multiphysics and Ansys Fluent, can simulate the motion of a single rising bubble in a stagnant liquid. Simulations were performed for spherical or slightly deformed bubbles (Db = 0.6, 0.8, and 1.5 mm) rising in water or in propanol. A simple 2D axisymmetric approach was used. Calculated bubble terminal velocities and bubble shape deformations were compared to both experimental data and theoretical estimations. Solver Comsol Multiphysics was able to precisely calculate the movement of smaller and larger bubbles; due to the 2D rotational symmetry, better results were obtained for small spherical bubbles. The deformation of larger bubbles was calculated sufficiently. Solver Ansys Fluent, in the setting used, failed to simulate the motion of small bubbles due to parasitic currents but allowed for modeling of the motion of larger bubbles. However, the description of the bubble velocity and shape was worse in comparison with experimental values.
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9

Ji, Hong, Wei Guo Zhu, Song Chen, and Jing Zhao. "Digital Analysis of Hydraulic Cone Valve Turbulence Based on Fluent 3D Solver." Applied Mechanics and Materials 385-386 (August 2013): 93–96. http://dx.doi.org/10.4028/www.scientific.net/amm.385-386.93.

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Анотація:
The hydraulic cone valve is an important basic component in Fluid drive and control technology. Characteristic of cone valve inner flow filed influences directly the valves performance. Especially when fluid flow in runner is turbulent, characteristics of flow field have great influence on the valves working performance.Main work of this paper is numerical calculation and simulation of cone valve inner runner flow field inside hydraulic hammer. First make a 3D modeling for cone valve using Pro/E, by fluent this paper analyses and discusses the distribution of hydraulic cone valve internal flow field including flow velocity field, pressure field and flow, etc when the cone valve core taper angle is 30°, the gap is 0.5 mm, and inlet velocity is different, analyses position and strength of the vortex, and finds out the main reason for energy consumption.The results of the study show that by the optimal design of the cone valve seat, the density degree of the flow and the size of the vortex is reduced, the energy loss is reduced, negative pressure zone also changes, the noise is reduced and the energy utilization is improved.
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Huang, Dennis, Zhigang Yang, and Randolph Chi Kin Leung. "Implementation of Direct Acoustic Simulation using ANSYS Fluent." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 263, no. 5 (August 1, 2021): 1243–52. http://dx.doi.org/10.3397/in-2021-1787.

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Анотація:
Direct Acoustic Simulation (DAS) is a powerful Computational Aero Acoustics method that obtains hydrodynamic and acoustic solutions simultaneously by solving compressible Navier-Stokes equation together with state equation of ideal gas. Thus, DAS has advantages for cases with flow acoustic coupling and high Mach numbers (). With an increasing demand of massive-scale calculations, a robust numerical solver for DAS is required. ANSYS Fluent is a suitable CFD platform with proven robustness. However, there is no direct implementation of DAS in the current version of ANSYS Fluent. The present study, therefore, aims to investigate an approach for implementing DAS using ANSYS Fluent. Given the acoustic part of fluctuations is much smaller than the hydrodynamic part in amplitude, a DAS solver requires high accuracy and low dissipation. Based on these needs, proper solution methods, spatial discrete methods and boundary conditions are firstly determined through simple calculations of two dimensional propagating plane waves. Afterwards aeroacoustics of a two-dimensional cavity flow at 0.6 is calculated to verify the capability for solving separating flow with the aforementioned set-up. Finally, aeroacoustics of a cylindrical bluff body at a turbulent regime and 0.2 is calculated in three-dimensions to verify the capability for solving turbulent flow using Monotonically Integrated Large Eddy Simulation.
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Більше джерел

Дисертації з теми "FLUENT SOLVER"

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Foltýn, Pavel. "Aerodynamická analýza a optimalizace konfigurace letounu ARES." Master's thesis, Vysoké učení technické v Brně. Fakulta strojního inženýrství, 2015. http://www.nusl.cz/ntk/nusl-232016.

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Анотація:
This thesis deals with the aerodynamic analysis and shape modifications of the ARES aircraft. The analysis focuses on the evaluation lift, drag, and pitching moment coefficient, and further to identify the locations of stripping stream which is characterized by high drag. Before the analysis calibration of the CFD solver is done with the model, which has been measured in the wind tunnel. The aim of calibration is to verify the accuracy and veracity of the methodology used in mesh creation and calculated values. Calculated values are compared with measured data. The shape modifications of the aircraft are focused on conceptual design of the suction inlets for cooling radiators and engine aircraft. Aerodynamic analysis is performed with the modified model in order to determine the variation of lift, drag and pitching moment coefficient from its original configuration.
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2

Bednář, Eduard. "Analýza vlivu proudění plynu v oblasti umístění vzorku v komoře enviromentálního rastrovacího elektronového mikroskopu." Master's thesis, Vysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií, 2016. http://www.nusl.cz/ntk/nusl-242067.

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Анотація:
This thesis deals with the simulation of fluid dynamics in environmental scanning electron microscope and evaluate solvers setup, the degree of discretization, choice of turbulent model and proposal optimal design of environmental scanning electron microscope. The theoretical part describes the issue of environmental scanning electron microscopy, software SolidWorks and ANSYS Fluent, basic equations describing fluid status, fluid turbulence, the mean free path of molecules and electron scattering. The practical part of the thesis is to create the model of environmental scanning electron microscope AQUASEM II in CAD system SolidWorks and simulation of fluid flow in the sample chamber before aperture PLA1 by ANSYS Fluent. A series of simulations provided the perfect setting solver. These knowledge are used in the second stage of the practical part, where is proposed optimal shape of the table sample and the input aperture PLA1.
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3

Acharya, Rutvika. "Investigation of Differences in Ansys Solvers CFX and Fluent." Thesis, KTH, Mekanik, 2016. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-203937.

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Анотація:
This thesis aims at presenting Computational Fluid Dynamics studies conducted on an axisymmetric model of the Siemens SGT-800 burner using Ansys Fluent, Ansys CFX and Ansys ICEM. The goal is to perform a mesh study and turbulence model study for isothermal flow. The result will show the differences observed while using the two solvers by Ansys, Fluent and CFX. Two different meshes, A, coarse and B, optimal have been used for the mesh study. This will reveal the mesh dependency of the different parameters and if any differences are observed between the solver’s convergence and mesh independency performance. To further validate the mesh independency, a simplified test case is simulated for turbulent flow for 32 different cases testing the numerical algorithms and spatial discretization available in Ansys Fluent and finding the optimal method to achieve convergence and reliable results. Turbulence model study has been performed where k-ε, k-ω and k-ω Shear Stress Transport (SST) model have been simulated and the results between solvers and models are compared to see if the solvers’ way of handling the different models varies.Studies from this thesis suggest that both solvers implement the turbulence models differently. Out of the three models compared, k-ω SST is the model with least differences between solvers. The solution looks alike and therefore it could be suggested to use this model, whenever possible, for future studies when both solvers are used. For the models k-ε and k-ω significant differences were found between the two solvers when comparing velocity, pressure and turbulence kinetic energy. Different reasons for its occurrence are discussed in the thesis and also attempts have been made to rule out few of the reasons to narrow down the possible causes. One of the goals of the thesis was to also discuss the differences in user-interface and solver capabilities which have been presented in the conclusions and discussions section of the report. Questions that still remain unanswered after the thesis are why these differences are present between solvers and which of the solvers’ results are more reliable when these differences have been found.
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Perez, Sancha David. "CFD analysis of a glider aircraft : Using different RANS solvers and introducing improvements in the design." Thesis, Linköpings universitet, Mekanisk värmeteori och strömningslära, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-159995.

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Анотація:
In this study, Computational Fluid Dynamics (CFD) simulations have been carried out in order to investigate and improve the performance of the Standard Cirrus glider, using different Navier-Stokes methods and solving the equations for the steady flow. The work has been divided in two parts: First, a study is performed to test the quality of the transition model (Gamma-ReTheta). The two dimensional results of the glider´s airfoil are compared against the results from panel’s methods and the open-source CFD codes: SU2 and OpenFoam. In addition, three dimensional glider´s models are simulated using the transition model with the purpose of creating a validated reference model of the glider’s performance in steady level flight. The simulations are carried out in two dimensions for the outer wing airfoil for a 1.5 e+06 Reynolds number and in three dimensions for the Wing & Fuselage model and Tail & Fuselage model under a range of velocities. Both simulations are validated against experimental data. In the second part of the study, the validated model is used to developed possible improvements in the glider´s external geometry that could produce possible benefits in the performance and handling qualities of the glider.
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5

Boga, Gabriele. "Analisi aerodinamica preliminare di un veicolo alimentato ad energia solare." Bachelor's thesis, Alma Mater Studiorum - Università di Bologna, 2017. http://amslaurea.unibo.it/14285/.

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Анотація:
L’obiettivo di questo lavoro è lo studio della variazione dei carichi aerodinamici per piccole variazioni della geometria su un veicolo da competizione ad energia solare. Questa analisi si inserisce nell’ottimizzazione aerodinamica di dettaglio. Il veicolo oggetto di studio è Emilia IV, auto sviluppata dal team Unibo Onda Solare. L’attività si è svolta tramite lo studio di tre configurazioni ottenute inclinando la parte superiore del veicolo originale di +2° e di -2°. Per le simulazioni fluidodinamiche è stato utilizzato il codice di calcolo commerciale Ansys Fluent. Le simulazioni sono state condotte con una velocità del flusso indisturbato di 20 m/s e con un numero di Reynolds calcolato sulla lunghezza della vettura di 6 milioni. Per la modellazione della turbolenza è stato utilizzato il modello k-epsilon realizable. È stato considerato uno strato limite turbolento per tutta la lunghezza del veicolo. La validazione del modello utilizzato è stata effettuata sulla geometria originale di Emilia IV tramite dati ottenuti precedentemente da simulazioni condotte con codici di calcolo Open Source (Open Foam) da ricercatori della Facoltà di Ingegneria di Forlì. La validazione della mesh è stata effettuata tramite simulazioni con quattro griglie di calcolo con numero di elementi crescente per verificarne la convergenza. Il numero di elementi della mesh definitiva è di 8 milioni composta da celle tetraedriche e da celle prismatiche. Si è data particolare rilevanza al coefficiente di resistenza delle tre vetture. Il modello utilizzato ha fornito risultatati sufficientemente accurati al fine di questo lavoro. La geometria originale si è dimostrata essere la più efficiente in termini di resistenza aerodinamica.
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6

Ohle, Andrea. "CO2-Abtrennung aus Gasströmen durch Absorption in Poly(methyldiglykol)amin." Doctoral thesis, Saechsische Landesbibliothek- Staats- und Universitaetsbibliothek Dresden, 2009. http://nbn-resolving.de/urn:nbn:de:bsz:14-qucosa-23497.

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Анотація:
In dieser Dissertation wird ein Prozess für die absorptive CO2-Abtrennung aus Gasströmen vorgestellt, der durch die Nutzung des neu entwickelten Waschmittels GenosorbN in einem Postcombustion-Prozess einen geringeren Energiebedarf als bisher bekannte Verfahren aufweist. Für die Nachrüstung bereits vorhandener Kraftwerke ist der Postcombustion-Prozess vorteilhaft, da er im Vergleich zum IGCC- oder dem Oxyfuel-Verfahren die geringsten Änderungen im Kraftwerksprozess selbst erfordert. Die bisher für die CO2-Abtrennung diskutierten Absorptionsmittel, wie z. B. MEA (Mono-Ethanol-Amin), haben allerdings vor allem in der Regeneration einen sehr hohen Energiebedarf, der vom Kraftwerk zusätzlich zur Verfügung gestellt werden muss. In Zusammenarbeit zwischen dem Institut für Verfahrenstechnik und Umwelttechnik der TU Dresden und der Clariant GmbH wurde das Absorptionsmittel GenosorbN (chemische Bezeichnung: Poly(methyldiglykol)amin) entwickelt. GenosorbN weist als Hybrid-Waschmittel gegenüber CO2 sowohl physikalische als auch chemische Bindungseigenschaften auf. Ausgehend von der Löslichkeitscharakteristik dieses Absorptionsmittels für CO2 und wichtigen Stoffwerten (z. B. Wärmekapazität und Lösungswärme von CO2) wurden mit Hilfe eines umfangreichen Versuchsprogramms an einer Technikumsanlage Betriebsparameter für einen energetisch günstigen technischen Einsatz ermittelt. Dabei hat sich herausgestellt, dass der Absorptionsprozess mit unverdünntem GenosorbN gegenüber einer MEA-Wäsche bei einem CO2-Abscheidegrad von ca. 90 % einen um ca. 20 - 27 % geringeren Energiebedarf in der Waschmittelregeneration aufweisen kann. Außerdem ist für die Desorption ein energetisch minderwertiger Heizdampf mit geringerem Temperatur- bzw. Druckniveau als bei dem MEA-Prozess ausreichend, da die Regenerationstemperatur um 40 - 50 K niedriger ist. Eine zusätzliche Druckabsenkung auf 400 mbar Absolutdruck im Desorber begünstigt die Regeneration deutlich
This dissertation presents a process for the absorptive CO2-separation from gas streams, which shows a lower energy requirement than established methods by using the newly developed absorption liquid GenosorbN in a postcombustion-process. To retrofit an already existing power plant, the postcombustion-process is advantageous, because it needs the least changes in the power plant-process itself compared to the IGCC- or the Oxyfuel-process. The absorbents discussed for the CO2-separation up to now, for example MEA (mono-ethanol-amine), cause a high energy requirement mainly in the solvent regeneration, which has to be provided additionally from the power plant. The solvent GenosorbN (chemical notation: poly(methyldiglycol)amine) was developed in cooperation between the Institute of Process Engineering and Environmental Engineering of the Technical University of Dresden and the Clariant GmbH. GenosorbN is a hybrid-absorbent and therefore it shows both physical and chemical bonding forces. Based on the solvents characteristic of solubility for CO2 and important data on chemical media (for example heat capacity and enthalpy of solution) operating parameters for an energetic advantageous technical application were identified by a lot of test series at a pilot plant. The measurements show that the absorption process with the undiluted GenosorbN has a circa 20 - 27 % lower energy demand for the solvent regeneration compared to the MEA-process to reach a degree of separation of 90 %. Furthermore a low-value heating steam with lower temperature and therefore lower pressure level suffices because of the significant lower (40 - 50 K) regeneration temperature. An additional pressure reduction to 400 mbar absolute pressure in the regeneration column favours the solvent regeneration considerably
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7

SHARMA, GIRI BHUSHAN. "CFD ANALYSIS OF COOLING TOWER WITH FLUENT SOLVER." Thesis, 2014. http://dspace.dtu.ac.in:8080/jspui/handle/repository/15417.

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Анотація:
A Cooling tower cools the working fluid using the principle of vaporization and sensible heat transfer. In this project the effect of design variables on Natural Draft Wet Cooling Tower has been observed using CFD analysis. The aim of the current work is to analyze the cooling tower and to observe that how the cooling range of tower depends on the various design parameters. The dependency of cooling range on fills design, rain zone height, air temperature and flow rate has been observed and conceptualized. This work also aims at determining the optimum fill height, optimum rain zone height for a design specific requirement. The problem has been solved in Discrete Phase Model using Lagrangian Particle Tracking and enabling the Stochastic Model with coupled heat and mass transfer and unsteady particle tracking assuming droplet collision and droplet breakup. The results shows that the cooling range increases as the fill height and the rain zone height is increased but there is more strong dependency on fill height rather than rain zone height. It is also observed that the range of the cooling tower increases as the flow rate of water is decreased. Its variation is observed and recorded in FLUENT 6. Theoretically it is observed and it is also clear from FLUENT 6 results that for a lower temperature the saturation pressure of water is also comparatively lower and so the driving force for the evaporation i.e. the difference of the saturation pressure and vapor pressure is also lower and so is the rate of evaporation. Hence a lower cooling is observed in rain zone for a higher depth of fills. The most of the factors affecting the cooling range are analyzed, recorded and compared for different sizes of the rain zone, different heights of fills, different mass flow rate, variable air temperature and an effort has been made for the optimization of the cooling tower.
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8

Xu, Wei 1986. "Numerical techniques for the design and prediction of performance of marine turbines and propellers." Thesis, 2010. http://hdl.handle.net/2152/ETD-UT-2010-08-2020.

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Анотація:
The performance of a horizontal axis marine current turbine is predicted by three numerical methods, vortex lattice method MPUF-3A, boundary element method PROPCAV and a commercial RANS solver FLUENT. The predictions are compared with the experimental measurements for the same turbine model. A fully unsteady wake alignment is utilized in order to model the realistic wake geometry of the turbine. A lifting line theory based method is developed to produce the optimum circulation distribution for turbines and propellers and a lifting line theory based database searching method is used to achieve the optimum circulation distribution for tidal turbines. A nonlinear optimization method (CAVOPT-3D) and another database-searching design method (CAVOPT-BASE) are utilized to design the blades of marine current turbines and marine propellers. A design procedure for the tidal turbine is proposed by using the developed methods successively. Finally, an interactive viscous/potential flow method is utilized to analyze the effect of nonuniform inflow on the performance of tidal turbines.
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Книги з теми "FLUENT SOLVER"

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Kleist, J. Olaf, Dimitra Dermitzaki, Bahar Oghalai, and Sabrina Zajak, eds. Gewaltschutz in Geflüchtetenunterkünften. Bielefeld, Germany: transcript Verlag, 2022. http://dx.doi.org/10.14361/9783839455449.

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Анотація:
Die kollektive Unterbringung von Asylsuchenden ist ein wichtiger Bestandteil der flüchtlingspolitischen Verwaltungspraxis in Deutschland. Bei aller Varianz der Art solcher Sammelunterkünfte sind damit stets auch prinzipielle Herausforderungen verbunden. Denn mit einem zentralen Raum zum Umgang mit Flucht und Ankunft werden zugleich Gefahren und Konflikte örtlich konzentriert. Parallel zur Entwicklung von Konzepten zur Bewältigung dieser Herausforderungen untersuchen die Beiträger*innen des Bandes die Lebensrealitäten in diesen Einrichtungen.
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2

Degradation of FEP thermal control materials returned from the Hubble Space Telescope. Greenbelt, Md: National Aeronautics and Space Administration, Goddard Space Flight Center, 1995.

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3

Barker, Howard, and Eduardo Houth. A Style and Its Origins. Bloomsbury Publishing Plc, 2007. http://dx.doi.org/10.5040/9781350924475.

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Howard Barker's alter-ego Eduardo Houth first materialised as the photographer of publicity images for Barker's theatre company The Wrestling School, one of many fictional identities assumed by the playwright to screen a range of his activities, including set and costume design. Writing of himself in the third person and in the historic tense, Barker/Houth achieves a fluency and an uncommon measure of objectivity, though objectivity is scarcely the sole intention. The result is a unique exercise in self-description, partisan but without the shrill self-justification so common in a mere autobiography. Barker/Houth's A Style and its Origins is very much a literary creation; it is also a totally original document and a rich history of the dramatist and his aesthetic.
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Частини книг з теми "FLUENT SOLVER"

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Tjoe, Hartono. "“Looking Back” to Solve Differently: Familiarity, Fluency, and Flexibility." In Mathematical Problem Solving, 3–20. Cham: Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-10472-6_1.

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Kretzschmar, M. "Temperature Dependence of the Flare Fluence Scaling Exponent." In Solar and Stellar Flares, 215–31. Dordrecht: Springer Netherlands, 2016. http://dx.doi.org/10.1007/978-94-024-0935-2_11.

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Smaus, Gerlinda. "Vom Sein zum Sollen - die Flucht nach vorne in die Generalprävention." In 22. Deutscher Soziologentag 1984, 287–89. Wiesbaden: VS Verlag für Sozialwissenschaften, 1985. http://dx.doi.org/10.1007/978-3-322-83518-5_93.

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Ullah, Hafiz Khadim, Sikiru Oluwarotimi Ismail, and Kumar Shantanu Prasad. "Assessment of Effectiveness of Hollow Fins for Performance Enhancement of Solar Still Device Using Simulation Approach." In Springer Proceedings in Energy, 145–55. Cham: Springer Nature Switzerland, 2023. http://dx.doi.org/10.1007/978-3-031-30960-1_15.

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AbstractUnavailability of relatively clean water for several industrial, domestic and agricultural purposes is a serious concern to many regions of the world today. This challenge is growing worse with the increasing world global warming and human population. Therefore, there is need to research into an innovative, sustainable and/or improved technology for an efficient and effective solution, such as desalination. Desalination of freely available sea water is considered a promising source of fresh water. Solar radiation is abundant and can be used to desalinate water, using a solar still device. Also, it is important to increase the productivity of the solar still device through hollow fin modification. Therefore, the effectiveness of this improvement was investigated in this study, using an analysis system (ANSYS) Fluent computational fluid dynamic (CFD) simulation. Appropriate models were used to describe the physical processes, including condensation, evaporation, multiphase flow, surface tension and solar radiation. A close agreement between the simulation values of solar energy and the water temperature in the basin was observed when compared with the experimental data from the literature. Velocity of 0.259 m/s, pressure of 55.8 Pa, temperature of 57.85 ºC and mass transfer rate of 1.41 kg/m3/s were obtained in the mid-plane of the improved double slope single basin (DSSB). The degree of improvement was 5–7% when compared with the existing models. Importantly, this process is economically efficient and can support the concepts of sustainability and healthy living, especially in rural areas.
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Cui, Jialin, Lijuan Li, Meng Zhang, Hongbing Liu, and Xianqiang Qu. "Dynamic Response Analysis of Floating Nuclear Power Plant Containment Under Marine Environment." In Springer Proceedings in Physics, 609–23. Singapore: Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-99-1023-6_53.

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AbstractFloating nuclear containment is in a harsher environment than conventional onshore nuclear containment. In view of the Marine environment under the condition of floating nuclear power plant containment structure safety, combined water dynamics and structural mechanics, considering the containment response under random movement of hull in the Marine environment, the influence of the containment structure load calculation, thus checking containment when working in pile structure safety, provide theoretical basis for the safe operation of floating nuclear power plants. In this paper, taking a floating nuclear power plant as an example, ANSYS 2021R1, Workbench, Fluent and other software of finite element analysis are used to conduct fatigue simulation of floating nuclear power plant. The time course curve of the 6-dof motion of the ship’s center of gravity is obtained, then, a remote displacement method is adopted to transfer the hull motion to the containment vessel to realize the numerical simulation of the containment vessel movement with the hull, thus to solve maximum normal stress and strain, the maximum load component of containment bearing under the action of Marine environmental load is obtained. The results show that the maximum stress and strain of the vessel increase obviously in the moving state compared with the static state of the vessel, which indicates that the random motion response of the vessel must be considered in the structural safety analysis of the floating nuclear power plant containment.
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Li, Chen, Peiting Sun, and Hongming Wang. "Effect of Leading-Edge Bulges on Aerodynamic Characteristics of Bionic Wingsail." In Advances in Transdisciplinary Engineering. IOS Press, 2021. http://dx.doi.org/10.3233/atde210340.

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The leading-edge bulges along the extension direction are designed on the marine wingsail. The height and the spanwise wavelength of the protuberances are 0.1c and 0.25c, respectively. At Reynolds number Re=5×105, the Reynolds Averaged Navier-Stokes equations are applied to the simulation of the wingsail with the bulges thanks to ANSYS Fluent finite-volume solver based on the SST K-ω models. The grid independence analysis is carried out with the lift and drag coefficients of the wingsail at AOA = 8° and AOA=20°. The results show that while the efficiency of the wingsail is reduced by devising the leading-edge bulges before stall, the bulges help to improve the lift coefficient of the wingsail when stalling. At AOA=22° under the action of the leading-edge tubercles, a convective vortex is formed on the suction surface of the modified wingsail, which reduces the flow loss. So the bulges of the wingsail can delay the stall.
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7

Kumar Gugulothu, Santhosh, B. Bhaskar, and V. V. Phani Babu. "Numerical Investigation of the Shock Train in a Scramjet with the Effects of Back-Pressure and Divergent Angles." In Numerical and Experimental Studies on Combustion Engines and Vehicles. IntechOpen, 2020. http://dx.doi.org/10.5772/intechopen.92555.

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Numerical simulations are carried out to study the effect of divergence angle and adverse pressure gradient on the movement of shock wave train in a scramjet isolator. The commercial software tool ANSYS Fluent 16 was used to simplify two dimensional Reynolds averaged Navier Stokes equation with compressible fluid flow by considering the density-based solver with standard K-ε turbulence model. The species transport model with single step volumetric reaction mechanism is employed. Initially, the simulated results are validated with experimental results available in open literature. The obtained results show that the variation of the divergence angle and back pressure on the scramjet isolator has greater significance on the flow field. Also, with an increase in the back pressure, due to the intense turbulent combustion, the shock wave train developed should expand along the length and also moves towards the leading edge of the isolator leading to rapid rise in the pressure so that the pressure at the entrance of the isolator can match the enhanced back pressures.
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Khan, Md Akhtar, and K. Vigneshwar. "Aerodynamic Analysis of Supersonic Spikes for Drag Reduction." In Global Perspectives on Robotics and Autonomous Systems, 130–67. IGI Global, 2023. http://dx.doi.org/10.4018/978-1-6684-7791-5.ch006.

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This research aims to examine the flow field over a NACA 651-412 aerofoil at a supersonic Mach number (M = 2) in the presence of a sharp spike and a Hemi spherical head spike. Using a spike integrated with an aerofoil alters the flow characteristics of the aerofoil, resulting in changes in aerodynamic lift and drag. Flow visualisation graphs and coefficients of aerodynamic drag and lift are measured. In this work, two spike designs were employed: sharp edges and hemispherical edges. The flow over an aerofoil with and without a spike is also compared in order to comprehend the performance of the NACA 6 series aerofoil with different geometry alteration. For computational simulation, ICEM CFD is used as a meshing tool and ANSYS fluent as an adjoint solver to analyse the external flow over the body. Furthermore, the drag increases significantly when the flight angle of attack increases. Employing certain installation angles effectively improves the drag reduction around the angle of attack and improve the lift-to-drag ratio.
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Claussen, Johann Hinrich. "Zwischengedanken: Was sollen wir tun?" In Das Buch der Flucht, 215–310. Verlag C.H.BECK oHG, 2018. http://dx.doi.org/10.17104/9783406726910-215.

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Koyunoğlu, Cemil. "Innovations in Heat Pump Design Using Computational Fluid Dynamics with Control Volume Method." In Modeling and Simulation in Engineering - Selected Problems. IntechOpen, 2020. http://dx.doi.org/10.5772/intechopen.93191.

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Mathematical modeling of the heat pump as a result of continuity, momentum, and energy equations is obtained. To solve these equations numerically, the problem is divided by a finite number of control volumes. Then the differential equations in these control volumes integrated and converted into algebraic equations. The importance of computational fluid dynamics in Industry 4.0 applications is to make current applications more efficient in heat pump applications. In this study, the book section is composed of the application of computational fluid dynamics by the control volume method using Ansys fluent program, which will benefit readers from industry 4.0 perspective, especially in energy efficiency issues according to the volume method of controlling correct heat pump designs.
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Тези доповідей конференцій з теми "FLUENT SOLVER"

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Berg, P., G. Janiga, and D. Thévenin. "CFD Challenge: Solutions Using the Commercial Solver Fluent and the Open-Source Solver OpenFOAM." In ASME 2012 Summer Bioengineering Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/sbc2012-80168.

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During the last decade, the research group in Magdeburg investigated the hemodynamics in cerebral aneurysms in close collaboration with experts from the fields of visualization and neuroradiology. Thanks to this, a considerable experience has been collected concerning unsteady blood flow simulation and analyses, involving a steadily increasing number of patient-specific aneurysms. Intermediate results have been presented at several VISC challenges. The simulations regarding this CFD Challenge as well as the post-processing have been carried out by the doctoral student Philipp Berg.
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Schaller, Jens, and Leonid Goubergrits. "CFD Challenge: Solutions Using the Commercial Finite Volume Solver, Fluent." In ASME 2012 Summer Bioengineering Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/sbc2012-80276.

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The Biofluid Mechanics Laboratory is working on hemodyanamics of medical devices and vessels — carotid bifurcations, coronary arteries and cerebral aneurysms — since mid 90s. For this challenge the simulations were performed by the doctorate student Jens Schaller supported by the student coworker Jan Osman using the commercial solver Fluent (Fluent 6.3.26, Ansys Inc., Canonsburg, USA).
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Kalsi, Hardeep S., and Quan Long. "CFD Challenge: Solutions Using the Commercial Finite Volume Solver, Fluent." In ASME 2012 Summer Bioengineering Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/sbc2012-80305.

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Mr. Kalsi is currently reading 3rd year Aerospace Engineering at Brunei University, London, this CFD challenge was undertaken as a final year dissertation project under the supervision of Dr. Quan Long at the Brunel Institute for Bioengineering (BIB). Simulations were carried out using the finite volume solver package ANSYS Fluent through the educational license available at Brunel University.
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Hodis, Simona, David F. Kallmes, and Dan Dragomir-Daescu. "CFD Challenge Solution Using the Commercial Finite Volume Solver Fluent." In ASME 2012 Summer Bioengineering Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/sbc2012-80564.

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The Modeling and Analysis group in the Division of Engineering at Mayo Clinic, Rochester works in the area of numerical modeling and experimental validation of cerebral aneurysms. In our modeling we use patient-specific geometries from imaging studies provided by Dr. Kallmes. The CFD analysis is performed with commercial packages Mimics (Materialise, Leuven, Belgium), for segmentation and ANSYS (ANSYS Inc. Canonsburg, PA) for meshing, simulation and post-processing. The experiments are conducted using a tomographic Particle Image Velocimetry system from LaVision Inc. The group is led by Dan Dragomir-Daescu, PhD and David F. Kallmes, MD and consists of two postdoctoral fellows and three engineers. For this project, CFD simulations were performed by postdoctoral fellow Simona Hodis, using the finite volume based solver Fluent.
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Aristokleous, Nicolas, Mohammad Iman Khozeymeh, Yannis Papaharilaou, Georgios C. Georgiou, and Andreas S. Anayiotos. "CFD Challenge: Solutions Using the Commercial Finite Volume Solver, Fluent." In ASME 2012 Summer Bioengineering Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/sbc2012-80691.

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This work is a collaborative effort between the Biomechanics and Living System Analysis Laboratory (BIOLISYS) in Cyprus and the Biomechanics Laboratory of IACM/FORTH in Greece. Both labs combine interdisciplinary skills from engineering, medicine and biology to provide solutions to clinical problems associated with cardiovascular and other diseases. For this study, numerical flow simulations were performed using: a) open source software VMTK and commercial software ICEM CFD as pre-processors, b) the finite volume based solver Fluent and c) Tecplot 360 (Amtec Inc.) for post-processing.
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Sen, Baris A., Yanhu Guo, Randal G. McKinney, Federico Montanari, and Frederick C. Bedford. "Pratt and Whitney Gas Turbine Combustor Design Using ANSYS Fluent and User Defined Functions." In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-70145.

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This paper summarizes work conducted at Pratt & Whitney to incorporate ANSYS Fluent into the computational fluid dynamics-based combustor design process. As a first step, turbulence, combustion and spray models that already exist and have been validated in the Pratt & Whitney legacy computational fluid dynamics (CFD) solver ALLSTAR were converted into user defined functions (UDFs) for usage with the core ANSYS Fluent solver. In this manner, a baseline solver was established that allowed a systematic testing of the ANSYS Fluent native models. The baseline solver was validated against computational results as well as experimental data obtained for (i) liquid jet in cross-flow (LJICF), (ii) ambient spray injector tests and (iii) Pratt & Whitney next generation product family configurations. These test cases established a thorough evaluation of ANSYS Fluent with UDFs on a spectrum of simple to complex geometries and flow physics relevant to the conditions encountered in aeroengine combustors. Results show that Fluent produces calculated results obtained by ALLSTAR with similar level of agreement to the experiments. Furthermore, Fluent provides better convergence compared to the legacy ALLSTAR solver with a similar computational resource requirement. The ANSYS Fluent native spray break-up models were also tested for the liquid jet in cross flow configuration, demonstrating the importance of modeling the stripping and primary break-up regime of a spray jet. This capability is currently available only via the use of UDFs.
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Bressloff, Neil W., and Ahsan T. Hameed. "CFD Challenge: Solutions Using the Mesher, Harpoon, and the Finite Volume Solver, Fluent." In ASME 2012 Summer Bioengineering Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/sbc2012-80007.

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The Bressloff group has focused on cardiovascular disease and its treatment for the last ten years. Possessing close ties with Southampton General Hospital, much of the work has sought understanding and/or solutions to clinically relevant problems, including the design of vascular stents. For the CFD Challenge, preliminary verification studies were performed by Masters student Ahsan Hameed using a fast hex-dominant mesher, Harpoon (Sharc Ltd) and V12.1.4 of the ANSYS Fluent solver (ANSYS, Inc.).
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Heinrich, Martin, and Rüdiger Schwarze. "All-Mach Number Density Based Flow Solver for OpenFOAM." In ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/gt2014-26220.

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A density-based solver for turbomachinery application is developed based on the central-upwind schemes of Kurganov and Tadmor using the open source CFD-library OpenFOAM. Preconditioning of Weiss and Smith is utilized to extend the applicability down to the incompressibility limit. Implicit residual averaging, bulk viscosity damping and local time stepping are employed to speed up the simulations. A low-storage 4-stage Runge-Kutta scheme and dual time-stepping are used for time integration. The presented solver is compared with results from ANSYS Fluent 13.0 and measurement data. Three different test cases are conducted to analyze different flow conditions: The circular bump for low and high speed inviscid flows and computational performance assessment, the two-dimensional VKI turbine guide vane for viscous flows and the the three-dimensional DLR high speed centrifual compressor validating the performance for rotating turbo-machinery. All three test cases show a very good agreement between OpenFOAM and ANSYS Fluent.
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9

Cito, S., J. Pallarés, A. Vernet, and I. Cuesta. "CFD Challenge: Giant Internal Carotid Artery Aneurysm Simulation Using the Commercial Finite Volume Solver Fluent." In ASME 2012 Summer Bioengineering Conference. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/sbc2012-80328.

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The main objective of ECoMMFiT is to advance in the knowledge of the structure of flows and their effect on the heat and mass transfer processes in problems with fundamental, clinical, industrial and environmental interest using experimental, computational and analytical tools. For this Challenge, CFD simulations were performed using the commercial finite-volume solver FLUENT 12 (ANSYS).
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10

Pang, Liping, and Baomin Sun. "3-D Numerical Simulation on Reheater Fouling in a Utility Boiler." In ASME/JSME 2004 Pressure Vessels and Piping Conference. ASMEDC, 2004. http://dx.doi.org/10.1115/pvp2004-3130.

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A numerical simulation investigation into the furnace and horizontal chimney process in a utility boiler is presented. The work is based on the commercial software FLUENT 6.1. Flow, chemistry, energy, conservation and radiation models are combined with the FLUNENT solver to simulate the process inside the furnace. Radiation and convection models are considered in the horizontal heater. The reheater is processed as a limited thickness heater and the convective heat transfer is considered in this numerical simulation. The temperature and velocity fields are calculated to unveil the process inside and outside the furnace. The result shows that the fouling in reheater is formed because of the temperature and velocity field in the flue gas passage. A limited test is done to validate the numerical simulation.
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Звіти організацій з теми "FLUENT SOLVER"

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PODDUBSKAYA, O., V. DARJINA, and E. MAKSIMKINA. PECULIARITIES OF STORITELLING APPLICATION FOR SPEECH DEVELOPMENT OF FUTURE FOREIGN LANGUAGE TEACHERS. Science and Innovation Center Publishing House, 2022. http://dx.doi.org/10.12731/2658-4034-2022-13-2-3-7-15.

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The article is devoted to the study of storytelling possibilities as a means of speech development, including the ones in a foreign language. This determines its relevance, since fluency in the word is necessary for a teacher to solve learning problems and create an atmosphere of interest, creativity and psychological contact with students.
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2

Schmid, Hansjörg, Julie Dubey, Tatiana Roveri, and Amir Sheikhzadegan. Muslimische Seelsorge in Bundesasylzentren. Vertiefte Evaluation des Pilotprojekts. Freiburg (Schweiz): Schweizerisches Zentrum für Islam und Gesellschaft (SZIG), Freiburg, 2023. http://dx.doi.org/10.51363/unifr.szigs.2023.008.

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Анотація:
Das Staatssekretariat für Migration (SEM) hat das im Frühjahr 2021 begonnene Pilotprojekt für muslimische Asylseelsorge bis Ende 2022 verlängert. Auf der Grundlage einer vertieften Evaluation durch das Schweizerische Zentrum für Islam und Gesellschaft (SZIG) der Universität Freiburg soll geprüft werden, wie sich muslimische Seelsorge dauerhaft einführen lässt. Das Ziel dieser Evaluation, die im Zeitraum von Juli bis Oktober 2022 realisiert wurde, war es, herauszufinden, wie sich die muslimische Seelsorge seit der letzten Evaluation entwickelt hat. Zudem war die Studie damit beauftragt, auch die im Januar 2022 eingeführte muslimische Seelsorge im Tessin zu evaluieren. Derzeit sind sechs muslimische Seelsorgende mit einem Stellenumfang von insgesamt 315% in elf Bundesasylzentren (BAZ) in den Asylregionen Westschweiz, Zürich, Ostschweiz sowie Tessin und Zentralschweiz im Einsatz. Die formativ angelegte qualitative Evaluation basiert auf Interviews und Hearings mit insgesamt 18 Personen (Seelsorgende, Verantwortliche P&A, SEM- Verantwortliche) sowie auf neuer wissenschaftlicher Literatur, Medienberichten und weiteren Dokumenten. Sie nimmt Bedürfnisse, Potenziale und Interaktionen unterschiedlicher Stakeholder in den Blick. Ein besonderes Augenmerk richtet sich dabei auf die Weiterentwicklung des Pilotprojekts im Jahr 2022. Die Studie kommt zum Schluss, dass sich die Befunde der letzten Evaluation bestätigen lassen und dass mit der zunehmenden Etablierung der muslimischen Seelsorge in den BAZ eine bessere Kooperation mit anderen Diensten in den Zentren wie auch eine grössere Wertschätzung dieser Dienstleistung von anderen Akteuren vor Ort einhergeht. Die Seelsorgenden begleiten die Gesuchstellenden, hören ihnen bei psychischen Belastungen oder gesundheitlichen Problemen zu, trösten sie in schwierigen Lebenssituationen, nehmen ihre religiösen Anliegen wahr und ermöglichen einen kultursensiblen Umgang mit einschneidenden Ereignissen in den BAZ. Darüber hinaus nehmen sie als Respektspersonen eine Mediationsrolle ein und tragen zur Vorbeugung von Konflikten bei. Muslimische Seelsorge erweist sich damit als wichtige Ressource, von der nicht nur die Gesuchstellenden, sondern auch die BAZ als ganze profitieren. Mehrere Befragte bekundeten, dass die muslimische Seelsorge nicht mehr aus den BAZ wegzudenken ist. So wurde in einem Fall auch das Angebot der muslimischen Seelsorge infolge einer Initiative des Betreuungspersonals auf ein weiteres BAZ ausgeweitet. Darüber hinaus konnte im zweiten Projektjahr die interreligiöse und interprofessionelle Zusammenarbeit mit den christlichen Seelsorgenden sowie mit dem Betreuungs-, Gesundheitsund Sicherheitspersonal vertieft werden. Der Quervergleich zeigt, dass die muslimische Seelsorge in den BAZ, in denen sie schon länger angeboten wird, besonders gut verankert ist. Im Tessin, wo erst Anfang 2022 ein muslimischer Seelsorgender seine Tätigkeit aufgenommen hat, besteht noch Bedarf an Information, Austausch und Rollenklärungen. In der Deutschschweiz arbeitet das SEM mit dem Verein QuaMS (Qualitätssicherung der Muslimischen Seelsorge in öffentlichen Institutionen) zusammen, der als Fachstelle an der Schnittstelle von öffentlichen Institutionen, Kanton und Religionsgemeinschaften breite Anerkennung geniesst. Aufgrund der Massnahmen zur Qualitätssicherung sowie der Supervisions- und Weiterbildungsmöglichkeiten für die Seelsorgenden im Rahmen von QuaMS ergibt sich hier ein Mehrwert, der in den anderen Sprachregionen so nicht gegeben ist. Die Evaluation empfiehlt mit Nachdruck eine Verstetigung des Pilotprojekts und schlägt einige Massnahmen zu deren Optimierung vor. So soll die strukturelle Verankerung und die Unabhängigkeit der muslimischen Seelsorgenden gestärkt werden. Dabei soll auch die spezifische Situation in den verschiedenen Sprachregionen berücksichtigt und der Austausch zwischen diesen intensiviert werden. Muslimische und kantonale Akteure in der Westschweiz sollen ermutigt werden, aufbauend auf dort vorhandene Kompetenzen eine analoge Organisation zu QuaMS zu schaffen. Ausserdem empfiehlt die Evaluation, ein besonderes Augenmerk auf die Diversität in den Seelsorgeteams zu richten, was Geschlecht, Sprachkenntnisse und konfessionelle Profile betrifft. Weiterbildungen für die Seelsorgenden sollen sich allgemeinen Herausforderungen im Zusammenhang mit Flucht und Asyl widmen, aber auch spezifischen Fragen Raum geben, die die kulturellen Kontexte und religiösen Ressourcen von Gesuchstellenden muslimischen Glaubens betreffen. Schliesslich sollen die Verantwortlichen der BAZ den Austausch mit allen Seelsorgenden intensivieren und im Rahmen von Workshops die Teamentwicklung vorantreiben. Aufgrund des anhaltend hohen Bedarfs soll auch geprüft werden, ob eine Erhöhung des Zeitbudgets der Seelsorgenden bzw. eine Anstellung weiterer Seelsorgender sowie eine Ausweitung auf weitere BAZ möglich ist.
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Zhou, Shaojun, and Marty Lail. Large Bench-Scale Development of a Non-Aqueous Solvent (NAS) CO2 Capture Process for Coal-fired Power Plants Utilizing Real Coal-Derived Flue Gas. Office of Scientific and Technical Information (OSTI), November 2019. http://dx.doi.org/10.2172/1579191.

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Lail, Marty. Large Bench-Scale Development of a Non-Aqueous Solvent (NAS) CO2 Capture Process for Coal-Fired Power Plants Utilizing Real Coal-Derived Flue Gas. Office of Scientific and Technical Information (OSTI), November 2019. http://dx.doi.org/10.2172/1578288.

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Ми пропонуємо знижки на всі преміум-плани для авторів, чиї праці увійшли до тематичних добірок літератури. Зв'яжіться з нами, щоб отримати унікальний промокод!

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