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Journal articles on the topic 'FLUENT SOLVER'

Author: Grafiati

Published: 11 September 2023

Last updated: 31 July 2025

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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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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 b

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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 (2016): 1155–62. http://dx.doi.org/10.2166/wst.2016.308.

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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

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Aziz, M. S. Abdul, M. Z. Abdullah, C. Y. Khor, et al. "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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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 PT

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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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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 othe

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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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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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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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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

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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 (2021): 452. http://dx.doi.org/10.3390/min11050452.

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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. Calc

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Farooque, Azam*, Jitendra Kumar Dr., and Javed Arham. "EXPERIMENTAL VALIDATION AND CFD PREDICTION OF NATURAL CONVECTION IN A VERTICAL PIPE USING FLUENT 14.5 SOLVER." INTERNATIONAL JOURNAL OF ENGINEERING SCIENCES & RESEARCH TECHNOLOGY 5, no. 3 (2016): 498–506. https://doi.org/10.5281/zenodo.47632.

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In this study, an experimental and CFD prediction of natural convection heat transfer in a vertical cylinder (pipe) is done by FLUENT 14.5 solver. Rosseland radiation model available in ANASYS CFD FLUENT 14.5 software will be investigate to find their usefulness for different parameters and cases as well as their limitation. Simulations will be performed with systematic parameterization to investigate the effect of changing models and parameters. Governing equations are solved using a finite volume method. The set up consist of brass cylinder with air as a working fluid. CFD results and experi

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10

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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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

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11

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 (2021): 1243–52. http://dx.doi.org/10.3397/in-2021-1787.

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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 stud

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12

Abdul Aziz, M. S., M. Z. Abdullah, and C. Y. Khor. "Effects of Solder Temperature on Pin Through-Hole during Wave Soldering: Thermal-Fluid Structure Interaction Analysis." Scientific World Journal 2014 (2014): 1–13. http://dx.doi.org/10.1155/2014/482363.

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An efficient simulation technique was proposed to examine the thermal-fluid structure interaction in the effects of solder temperature on pin through-hole during wave soldering. This study investigated the capillary flow behavior as well as the displacement, temperature distribution, and von Mises stress of a pin passed through a solder material. A single pin through-hole connector mounted on a printed circuit board (PCB) was simulated using a 3D model solved by FLUENT. The ABAQUS solver was employed to analyze the pin structure at solder temperatures of 456.15 K (183°C) <T< 643.15 K (37

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Feng, Kun, Chunqing Li, Ming Zhang, and Xuting Liu. "Simulation and Computational Study of CFD on Tube MBR Membrane Assembly." Discrete Dynamics in Nature and Society 2021 (May 13, 2021): 1–8. http://dx.doi.org/10.1155/2021/5577715.

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When using tubular MBR to treat sewage, the water production is an important parameter to measure the efficiency of the tubular MBR system. The problem to be solved in this paper is to calculate the water yield of the tubular MBR system, so as to evaluate the sewage treatment efficiency of the MBR system. This research uses the CFD simulation software ANSYS 16.0 to study the water yield of the tubular MBR system. The MBR model of a single membrane filament tube was established using the ICEM CFD preprocessor in ANSYS 16.0, and the structured grid was divided to obtain a grid file. Then, the fl

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Vyroubal, Petr, and Martin Mačák. "Numerical Modeling of Cyclic Voltametry." ECS Transactions 105, no. 1 (2021): 561–66. http://dx.doi.org/10.1149/10501.0561ecst.

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This paper deals with a new approach to numerical modeling of cyclic voltammetry using the CFD solver FLUENT. The standard use of this solver is in the field of flow and heat transfer calculations, however, it is possible to model electrochemical reactions and it also includes basic models for calculations related to batteries, such as charging and discharging processes, temperature fields, etc. Thanks to the possibility of scripting, however, it is possible to extend these tasks to a much more complex level.

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15

Abas, Aizat, N. Hafizah Mokhtar, M. H. H. Ishak, M. Z. Abdullah, and Ang Ho Tian. "Lattice Boltzmann Model of 3D Multiphase Flow in Artery Bifurcation Aneurysm Problem." Computational and Mathematical Methods in Medicine 2016 (2016): 1–17. http://dx.doi.org/10.1155/2016/6143126.

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This paper simulates and predicts the laminar flow inside the 3D aneurysm geometry, since the hemodynamic situation in the blood vessels is difficult to determine and visualize using standard imaging techniques, for example, magnetic resonance imaging (MRI). Three different types of Lattice Boltzmann (LB) models are computed, namely, single relaxation time (SRT), multiple relaxation time (MRT), and regularized BGK models. The results obtained using these different versions of the LB-based code will then be validated with ANSYS FLUENT, a commercially available finite volume- (FV-) based CFD sol

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16

Zhao, Zhongping, Ruiping Xiong, Junhong Yang, and Xing Hu. "A research of numerical simulation on argon magnetic fluid." Thermal Science, no. 00 (2024): 195. http://dx.doi.org/10.2298/tsci240502195z.

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An argon magnetic fluid is a collection of free charged particles moving in random directions especially that is a weakly ionized argon discharge and on the average, electrically neutral. Two-dimensional numerical steady-state model of an argon magnetic fluid generator is presented to investigate the thermodynamic behaviors and the distribution of current density. Computational fluid dynamics codes, OpenFOAM and Fluent, are utilized in a modified form to model the argon magnetic flow inside the generator. Modeling a thermal magnetic fluid requires a combination of mutually related fluid dynami

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17

Velkova, Cvetelina. "AN ESTIMATION OF THE HYDRODYNAMIC FLOW FIELD (HDFF) AROUND A SPHERE THROUGH CFD AND EXPERIMENT." ENVIRONMENT. TECHNOLOGIES. RESOURCES. Proceedings of the International Scientific and Practical Conference 3 (June 22, 2024): 325–29. http://dx.doi.org/10.17770/etr2024vol3.8119.

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In the presented study is made a numerical modelling of the hydrodynamic flow field (HDFF) around a sphere. Numerical modelling has been made using the software ANSYS Workbench and the calculation of the hydrodynamic flow field (HDFF) around a sphere was implemented using the solver ANSYS Fluent. The analysis of HDFF around the sphere has realized using Finite Element Method (FEM) available in the ANSYS Fluent environment. The HDFF has examined around the sphere at a given horizon using the real flow, the fluid is water. The obtained numerical results for velocities and pressures around the sp

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18

Nguyen, Phu Khanh, Koichi Mori, Thi Kim Dung Hoang, Van Hoa Nguyen, and Hai Anh Nguyen. "Research on Simulation and Experiment of Dynamic Aeroelastic Analysis on Wing Structure." Applied Mechanics and Materials 798 (October 2015): 541–45. http://dx.doi.org/10.4028/www.scientific.net/amm.798.541.

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In this paper, a simulation method was realized to predict aeroelastic response and characteristic parameters of wing structure. This method was developed base on interaction between Fluent solver and Mechanical APDL solver using a coupling system in ANSYS Workbench. AGARD 445.6 wing model was chose for this developed procedure at high speed. Obtained results were compared to other numerical result and experimental results. After that, experiment was also setup in suitable conditions to study aeroelacticity characteristics and specify quantitative parameters as frequency, amplitude of oscillat

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19

Conde, J. M. P., and M. B. S. P. Condeço. "Numerical Simulation of an Oscillating Water Column (OWC) Wave Energy Converter (WEC) on a Breakwater Using OpenFOAM^®." Defect and Diffusion Forum 396 (August 2019): 12–21. http://dx.doi.org/10.4028/www.scientific.net/ddf.396.12.

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This paper presents the application of the OpenFOAM® software package, using the IHFoam/OlaFlow solver, in the simulation of the water waves and air flow in an OWC-WEC located on a breakwater, the Mutriku power station in the north of Spain. The numerical code solves the transient Reynolds averaged Navier-Stokes (RANS) equations, using the Volume of Fluid (VoF) technique to identify the free surface. The standard k-ε turbulence model was used evaluate the Reynold stresses. Two geometries were considered: one with the pneumatic chamber completely open to the atmosphere; and other with the chamb

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20

Das Sahu, Kapil, Shyam Sunder Yadav, and Mani Sankar Dasgupta. "A Comparison of Classical Nucleation Theory and Thermal Phase Change Based Condensation Models." Journal of Physics: Conference Series 2818, no. 1 (2024): 012016. http://dx.doi.org/10.1088/1742-6596/2818/1/012016.

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Abstract In this work, we perform numerical simulations of the condensation process of CO2 inside a converging-diverging nozzle. We use Ansys Fluent for the simulation work. The real gas properties of CO2 are generated in tabular form (including metastable states) using NIST Refprop. We compare the distribution of physical quantities during the high-speed, compressible flow of CO2 inside a nozzle under the Classical Nucleation Theory (CNT) and the Thermal Phase Change (TPC) models. The CNT model is known to be accurate but computationally expensive while the TPC model is computationally cheape

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SEENI, Aravind, Parvathy RAJENDRAN, Mamat HUSSIN, and Farzad ISMAIL. "Errors and uncertainties in simulation of steady, viscous flow past a circular cylinder at Re = 20 using a systematic approach." INCAS BULLETIN 12, no. 3 (2020): 203–17. http://dx.doi.org/10.13111/2066-8201.2020.12.3.17.

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The use of Computational Fluid Dynamics as a tool for design and analysis of aerospace systems is well established. Since the results generated by a CFD solver are numerical approximations, the solution is inherently produced with errors and uncertainties. In this paper, a simple fluid flow problem of laminar, incompressible flow past a circular cylinder at Reynolds number of 20 is allowed to be solved by the well-known finite-volume solver ANSYS Fluent. The effect of variations in mesh resolution, domain boundary location and residual criteria settings is investigated. For all the cases, fini

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Horová, Veronika, Marian Bojko, and Josef Dobeš. "Methodology of using the Adjoint solver optimization tool during flow in the intercooler filling line to minimize pressure drop." EPJ Web of Conferences 213 (2019): 02025. http://dx.doi.org/10.1051/epjconf/201921302025.

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The paper deals with numerical modelling of the flow in the intercooler filling line by Adjoint solver to minimize pressure loss. The ANSYS Fluent software was used for the calculations. The basic flow calculation was performed in the first phase. Then the mathematical model with Adjoint solver optimization tool was defined. The numerical calculation was unstable and did not lead to a convergent solution, because of creation of vortexes. The mathematical model was simplified in the second phase. To suppress instabilities and vortices a dynamic viscosity of coolant was adjusted. The pressure gr

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Peter, Ildiko, and Mario Rosso. "Simulation of Electrodeposition of Al from Ionic Liquid." Materials Science Forum 794-796 (June 2014): 229–34. http://dx.doi.org/10.4028/www.scientific.net/msf.794-796.229.

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Galvanic deposition of Aluminium on steel substrate, starting from liquid ions, is considered. How the agitation of the liquid during deposition influences the homogeneity of the developed coating layer is investigated by a commercially available FLUENT® ANSYS® solver. Comparison of data coming from numerical simulation with experimentally obtained results are presented. The reported results demonstrate that the deposition process parameter influences the quality of the deposited aluminium.

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Chen, Ye, Zhongxi Hou, Bingjie Zhu, Zheng Guo, and Boting Xu. "Validation for Aerodynamic Performance on Over-Expanded State of Single Expansion Ramp Nozzle Configuration." Aerospace 9, no. 11 (2022): 715. http://dx.doi.org/10.3390/aerospace9110715.

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The performance of a single expansion ramp nozzle (SERN) drastically declines on over-expanded conditions. A numerical code can accurately predict nozzle performance in the over-expanded state, which is crucial for the SERN configuration design. A Reynolds-averaged Navier–Stokes (RANS) simulation of the SERN jet in an over-expanded state was performed to verify the numerical performance of the well-established commercial CFD solver (ANSYS FluentTM v202) and rhoCentralFoam solver in OpenFOAM. The wall pressure distributions and flow field characteristics including the shock structures and the w

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Czerwiński, Grzegorz, and Jerzy Wołoszyn. "Optimization of Air Cooling System Using Adjoint Solver Technique." Energies 14, no. 13 (2021): 3753. http://dx.doi.org/10.3390/en14133753.

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Air cooling systems are currently the most popular and least expensive solutions to maintain a safe temperature in electronic devices. Heat sinks have been widely used in this area, allowing for an increase in the effective heat transfer surface area. The main objective of this study was to optimise the shape of the heat sink geometric model using the Adjoint Solver technique. The optimised shape in the context of minimal temperature value behind the heat sink is proposed. The effect of radiation and trapezoidal fin shape on the maximum temperature in the cooling system is also investigated. S

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26

Zhao, Zihan, Lingxiao Tang, and Yiqing Xiao. "Simulation of the Neutral Atmospheric Flow Using Multiscale Modeling: Comparative Studies for SimpleFoam and Fluent Solver." Atmosphere 15, no. 10 (2024): 1259. http://dx.doi.org/10.3390/atmos15101259.

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The reproduced planetary boundary layer (PBL) wind is commonly applied in downscaled simulations using commercial CFD codes with Reynolds-averaged Navier–Stokes (RANS) turbulence modeling. When using the turbulent inlets calculated by numerical weather prediction models (NWP), adjustments of the turbulence eddy viscosity closures and wall function formulations are concerned with maintaining the fully developed wind profiles specified at the inlet of CFD domains. The impact of these related configurations is worth discussing in engineering applications, especially when commercial codes restrict

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27

Ji, Hong, Wei Guo Zhu, Song Chen, and Jing Zhao. "Analysis of the Laminar Flow in the Hydraulic Poppet Valve Based on the Fluent 3D Solver." Applied Mechanics and Materials 385-386 (August 2013): 97–100. http://dx.doi.org/10.4028/www.scientific.net/amm.385-386.97.

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The hydraulic poppet valve is an important basic component in Fluid drive and control technology, whose characteristic of the inner flow filed influences directly the valves performance. The main work is numerical calculation and simulation of flow field inside the cone valve in the hydraulic hammer. The first step is 3d modeling of cone valve. By using fluent software the study analyses and discusses the flow field of hydraulic cone valve including flow velocity field, pressure field and flow line distribution when the valve cores cone angle is 30°, analyses the cause of the vortexes position

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Premjiyani, Hemex, Arunesh Dwivedi, and Hiren Rana. "MODELING AND ANALYSIS OF PRESSURE DROP IN FLUE GAS DUCT PATH USING COMPUTATIONAL FLUID DYNAMICS." International Journal of Advanced Research 13, no. 04 (2025): 845–54. https://doi.org/10.21474/ijar01/20787.

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Nowadays, in contrast to the worldwide energy crisis and the global commitment to mitigate carbon footprints from the source, energy conservation and carbon emission reduction are vital and mandatory for almost all entities hence, so for coal based thermal power stations. Higher auxiliary power consumption than the optimum value is observed in almost all power plant auxiliaries, starting from the boiler feed pump to the induced draft fans during the energy audit. Also, the oldness of the power plant worsens this scenario of high auxiliary power consumption. Hence, any modification in the desig

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Ding, F., C. B. Shen, W. Huang, and J. Liu. "Numerical validation and back-pressure effect on internal compression flows of typical supersonic inlet." Aeronautical Journal 119, no. 1215 (2015): 631–45. http://dx.doi.org/10.1017/s0001924000010721.

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AbstractA numerical study was conducted to analyse the performance of different turbulence models and different turbulence intensities and turbulence length scales specified for the boundary condition of the inflow to the internal compression flow field of a typical supersonic inlet. The effect of the back-pressure ratio on the properties of the flow field was also investigated. Computational results obtained by the commercial software FLUENT, which is used to solve the full two-dimensional Reynolds-averaged Navier-Stokes equations, were validated through both graphical and quantitative compar

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Malik, F. Elmzughi, A. Hamoudah Mohammed, and Omar Almuhaddibi Tawfeeq. "Design and performance simulation of a soft artificial heart by using the ANSYS software." i-manager’s Journal on Future Engineering and Technology 19, no. 2 (2024): 1. http://dx.doi.org/10.26634/jfet.19.2.20487.

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Blood is pumped from the heart, a muscular organ, to various body organs via blood arteries. The aim of this paper is to create a temporary device, such as a pump, for individuals with cardiac diseases for whom survival without a transplant is unfeasible. Until a donor heart becomes available, the patient may have ample time with these makeshift devices. This paper uses engineering principles to explore the idea of an artificial heart. Using SOLIDWORKS 18 and ANSYS 21, numerical simulation and examination of the artificial heart were carried out. A Multiphysics static structural model and flue

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Zuppardi, G., and D. Paterna. "Influence of rarefaction on the computation of aerodynamic parameters in hypersonic flow." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 216, no. 6 (2002): 277–90. http://dx.doi.org/10.1243/095441002321029026.

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The results from two well-known and widely accepted codes, the Navier—Stokes solver FLUENT and the direct simulation Monte Carlo (DSMC) solver DS2G, have been analysed in order to fix the levels of the flow field rarefaction where the codes can work properly for the computation of aerodynamic forces and heat flux on a spacecraft during the re-entry. This subject has already been widely investigated; thus the purpose of the present work is to provide a further contribution. In order to make realistic computations, a probable path of a typical capsule, returning from an interplanetary mission to

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Liu, Zhuoran, Caizheng Wang, Ke Zhang, Zhuo Zhao, and Zhifeng Xie. "Research on Computational Method of Supersonic Inlet/Isolator Internal Flow." Applied Sciences 11, no. 19 (2021): 9272. http://dx.doi.org/10.3390/app11199272.

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In this research, a CFD solver is developed for solving the 2D/3D compressible flow problem: the finite volume method based on multi-block structural grids is used to solve the compressible Reynolds averaged Navier–Stokes equations (RANS). Included in the methodology are multiple high-order reconstruction schemes, such as the 3rd-order MUSCL (Monotone Upstreamcentered Schemes for Conservation Laws), 5th-order WENO (Weight Essentially Non-Oscillatory), and 5th-order MP (Monotonicity-Preserving) schemes. Of the variety of turbulence models that are embedded, this solver is mainly based on the sh

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Abdul Aziz, M. S., M. Z. Abdullah, and C. Y. Khor. "Thermal fluid-structure interaction of PCB configurations during the wave soldering process." Soldering & Surface Mount Technology 27, no. 1 (2015): 31–44. http://dx.doi.org/10.1108/ssmt-07-2014-0013.

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Purpose – This paper aims to investigate the thermal fluid–structure interactions (FSIs) of printed circuit boards (PCBs) at different component configurations during the wave soldering process and experimental validation. Design/methodology/approach – The thermally induced displacement and stress on the PCB and its components are the foci of this study. Finite volume solver FLUENT and finite element solver ABAQUS, coupled with a mesh-based parallel code coupling interface, were utilized to perform the analysis. A sound card PCB (138 × 85 × 1.5 mm3), consisting of a transistor, diode, capacito

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Nagy, Csaba, Arnold Rónaföldi, and András Roósz. "Comparison of Measured and Numerically Simulated Angular Velocity of Magnetically Stirred Liquid Ga-ln Alloy." Materials Science Forum 752 (March 2013): 157–66. http://dx.doi.org/10.4028/www.scientific.net/msf.752.157.

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A measurement of the angular velocity/revolution number of magnetically stirred liquid gallium-indium alloy was realized with newly developed angular velocity measuring equipment. To get additional information about the flow of the melt, a numerical simulation model was performed with ANSYS FLUENT 13.0 with a single phase 2D k-ε turbulence solver. The aim was to reproduce the flow as accurate as possible, so the measured and computed angular velocity data was compared, to see if the system can be modeled fairly well.

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Maram, Moloud Arian, Hamid Reza Ghafari, Hassan Ghassemi, and Mahmoud Ghiasi. "Numerical Study on the Tandem Submerged Hydrofoils Using RANS Solver." Mathematical Problems in Engineering 2021 (February 10, 2021): 1–17. http://dx.doi.org/10.1155/2021/8364980.

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This paper is presented on the tandem two-dimensional hydrofoils with profiles NACA4412 in single-phase and two-phase flow domains for different submergence depths and different distances in a various angle of attack (AoA). Also, supercavitation is studied at σ = 0.34 by the Zwart cavitation model. Reynolds-averaged Navier–Stokes (RANS) with the shear stress transport (SST) K-ω is employed as a turbulence model in transient analysis of Ansys FLUENT software. The numerical results show that, by increasing depth, the drag coefficient increases for both hydrofoils 1 and 2 as well as the lift coef

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Robert, Rivaldo Anderson, Made Sucipta, I. Made Widiyarta, Cindy Dwi Meylinda, and Betty Florensia Sinaga. "Aerodynamic Analysis of Obhi-Mec Unud Bio-Hybrid Electric Vehicle Using Computational Fluid Dynamics." Journal of Physics: Conference Series 2972, no. 1 (2025): 012033. https://doi.org/10.1088/1742-6596/2972/1/012033.

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Abstract The aerodynamic properties of a vehicle are a factor in vehicle body development, such as the drag force, lift force, and flow pattern that occurs on the vehicle body. Using computational fluid dynamics (CFD), such as ANSYS Fluent, those properties can be investigated to design and analyze in many applications. Obhi-Mec Unud Bio-Hybrid is one of the electric vehicles developed to support the decarbonization program investigated through the fluid flow phenomenon to evaluate the drag and lift forces. The ANSYS Fluent with a realizable k-epsilon flow model with a pressure-based solver an

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Younoussi, Somaya, and Abdeslem Ettaouil. "Numerical Study of a Small Horizontal-Axis Wind Turbine Aerodynamics Operating at Low Wind Speed." Fluids 8, no. 7 (2023): 192. http://dx.doi.org/10.3390/fluids8070192.

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The present work aims to study the aerodynamic characteristics of a newly designed three-bladed horizontal-axis wind turbine (HAWT) using the Computational Fluid Dynamic (CFD) method. The blade geometry is designed using an improved Blade Element Momentum (BEM) method to be similar in size to the Ampair300 wind turbine. The shear stress transport (SST) transition turbulence model closure is utilized to solve the steady state three-dimensional Reynolds Averaged Navier-Stokes (RANS) equations. The Ansys Fluent CFD solver is used to solve the problem. Then, a comparison between the two turbines’

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Saha, Pritam, and Harshpreet Singh Kaberwal. "Numerical Analysis of Aerodynamic Performance Characteristics of NACA 2312 and NACA 2412." Volume 5 - 2020, Issue 3 - March 5, no. 3 (2020): 420–28. http://dx.doi.org/10.38124/ijisrt20mar229.

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Comparison of the Aerodynamic Performance characteristics of NACA 2312 and NACA 2412 aerofoils under the same flow conditions at a Reynolds number of 2.74 x 106 is presented. ANSYS is used for the creation of geometry and meshing and FLUENT is used as a solver. Coefficient of lift and coefficient of drag for both aerofoils are compared for a range of Angle of Attack while the free stream velocity of air is kept constant. This analysis can be used for the wing design and other aerodynamic modelling corresponds to these aerofoils.

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THIELSCHER, MICHAEL. "FLUX: A logic programming method for reasoning agents." Theory and Practice of Logic Programming 5, no. 4-5 (2005): 533–65. http://dx.doi.org/10.1017/s1471068405002358.

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FLUX is a programming method for the design of agents that reason logically about their actions and sensor information in the presence of incomplete knowledge. The core of FLUX is a system of Constraint Handling Rules, which enables agents to maintain an internal model of their environment by which they control their own behavior. The general action representation formalism of the fluent calculus provides the formal semantics for the constraint solver. FLUX exhibits excellent computational behavior due to both a carefully restricted expressiveness and the inference paradigm of progression.

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Hangargekar, Sunvil, Sreedhar Reddy, Gang Wang, and Scott Hausmann. "Numerical and Experimental Investigation of Aerodynamic Noise Generated by Subsonic Axial Fan Using Hybrid Approach." NAFEMS International Journal of CFD Case Studies 13, no. 1 (2023): 31–41. http://dx.doi.org/10.59972/nh4vqxbv.

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This research work reports the study and investigation of aerodynamically generated noise characteristics of the fan using a hybrid numerical approach. Numerical results are compared with the experimental results. The experiment is conducted to determine the sound power radiated by the fan. This experiment is carried out in the reverberant and anechoic chambers as a test environment. The axial subsonic fan is considered for the study. Detailed experimental work is reported in the first section, and in the second section, numerical simulation results are reported. Flow analysis is carried out u

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AbdelGawad, Alaa R., and Liang Guozhu. "A Numerical Simulation Study for A Dual Thrust Solid Propellant Rocket Motor Nozzle." Journal of Physics: Conference Series 2235, no. 1 (2022): 012010. http://dx.doi.org/10.1088/1742-6596/2235/1/012010.

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Abstract CFD simulation through the rocket motor nozzle is an important issue as it gives a better understanding of the flow behavior and shows the evolution of the parameters along with the nozzle. CFD simulations using ANSYS FLUENT were conducted to model the flow through an experimental dual thrust solid rocket motor nozzle at two pressure values representing the two pressure levels. A two-dimensional axisymmetric numerical simulation was carried out using a pressure-based solver to solve the governing equation and the standard k-ε model to model the turbulence through the motor nozzle. The

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Reshma Sett, Prathmesh Pravin Verekar, and Mohammad Zuber. "Comparative Study of Dimple Effect on Three-Dimensional Cambered Aircraft Wing." Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 104, no. 2 (2023): 115–26. http://dx.doi.org/10.37934/arfmts.104.2.115126.

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This paper focuses on aerodynamic analysis over a 3D cambered wing with dimple-like surface modification. Application of the golf ball dimples on airfoils is predicted to be a good alternative for drag reduction. A golf ball with dimples allows for smooth and controlled flight. Models of cambered wings based on NACA 2412 airfoil were created to investigate the dimple effect. A comparative study is carried out between wing models with inward and outward dimples at 50% of chord length locations. Simulations were conducted for two velocities – 30 m/s and 90 m/s and the angle of attacks varying fr

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Danaila, Sterian, Delia Teleaga, and Luiza Zavalan. "Finite Volume Particle Method for Incompressible Flows." Applied Mechanics and Materials 656 (October 2014): 72–80. http://dx.doi.org/10.4028/www.scientific.net/amm.656.72.

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This paper presents an application of the Finite Volume Particle Method to incompressible flows. The two-dimensional incompressible Navier-Stokes solver is based on Chorin’s projection method with finite volume particle discretization. The Finite Volume Particle Method is a meshless method for fluid dynamics which unifies advantages of particle methods and finite volume methods in one scheme. The method of manufactured solutions is used to examine the global discretization error and finally a comparison between finite volume particle method simulations of an incompressible flow around a fixed

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Stalewski, Wieńczysław, and Katarzyna Surmacz. "Helicopter Flight Simulation based on URANS Solver and Virtual Blade Model." Journal of KONES 26, no. 3 (2019): 211–17. http://dx.doi.org/10.2478/kones-2019-0075.

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Abstract The methodology of simulation of a rotorcraft flight has been developed and applied to simulate several stages of flight of light helicopter. The methodology is based on coupling of several computational models of Computational Fluid Dynamics, Flight Dynamic. The essence of the methodology consists in calculation of aerodynamic forces acting on the flying rotorcraft by solving during the simulation the Unsteady Reynolds-Averaged Navier-Stokes (URANS) equations. In this approach, the rotorcraft is flying inside the computational 3D mesh modelling the space filled with the air. The flig

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Młynarczyk, Przemysław. "The influence of the numerical solver selection on the nozzle impulse flow simulation results." MATEC Web of Conferences 240 (2018): 03008. http://dx.doi.org/10.1051/matecconf/201824003008.

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Numerical simulations are currently used for different applications in a various fields of science. Certain solutions are not as obvious as the others while the results can give very valuable conclusions. Computational Fluid Dynamics (CFD) is one of the tools that can be used to solve different problems related with the mass and heat transfer. Nowadays it is already known that the impulse flow simulation allows to determine pressure pulsation attenuation parameters by a given geometry. However, the nozzle shape optimization method strongly depends on the numerical results obtained from the imp

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Jia, Liyuan, Song Sang, Xiao Shi, and Fukui Shen. "Investigation on Numerical Simulation of VIV of Deep-Sea Flexible Risers." Applied Sciences 13, no. 14 (2023): 8096. http://dx.doi.org/10.3390/app13148096.

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The vortex-induced vibration (VIV) of flexible risers is a complex fluid–structure interaction (FSI) phenomenon. In this study, we conducted a numerical simulation method based on the slicing method to study the vortex-induced vibration (VIV) of deep-sea flexible risers with different slenderness ratios and uniform flow velocities. The method combines the finite element model of the riser structure with the two-dimensional flow field slices solved by the Fluent solver. The fluid–structure interaction was realized by a self-compiled UDF program and the overset mesh technique. The numerical resu

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Sugar, Mitchell, and Paul Slaboch. "Directivity of sound propagation from an commercial supersonic engine inlet." INTER-NOISE and NOISE-CON Congress and Conference Proceedings 263, no. 2 (2021): 4211–18. http://dx.doi.org/10.3397/in-2021-2633.

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The effects of mean flow variations on sound propagation from an axisymmetric commercial supersonic engine inlet were studied using numerical methods. A finite element model of the inlet was constructed in Ansys Fluent and used to solve for flow fields given by different initial conditions. Results from this model were fed into the aeroacoustic solver, Actran, and used to calculate far field radiated noise as well as the directivity of that noise. The acoustic source of this noise was a plane wave of a known strength placed at the fan face. In addition to assessing the effects of mean flow on

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Wang, Yun, Bing Nan Li, Zhen Ying Xu, and Yong Kang Zhang. "The Analysis of Wave Form for 3-D Wave Tank." Advanced Materials Research 463-464 (February 2012): 1392–96. http://dx.doi.org/10.4028/www.scientific.net/amr.463-464.1392.

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The 3-D numerical model of wave tank is developed considering the effects of wave generating and absorbing based on viscous fluid motion differential equations (N-S equation) and the volume of fluid (VOF) method by the use of FLUENT solver. The simulation is also made by the analysis of the existing methods of wave simulation. The wave form of the 3-D wave tank is analyzed with the result of diverse diversification at different wave location and their relationship. The flow path of each particle of the wave during the propagation is also been analyzed, which provides guidance for the wave form

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Karaman, Mehmet, Ibrahim Özkol, and Güven Kömürgöz. "Heat Transfer Enhancement in Turbine Blade Internal Cooling Ducts." Advanced Materials Research 1016 (August 2014): 743–47. http://dx.doi.org/10.4028/www.scientific.net/amr.1016.743.

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Gas turbine is a type of rotary engine that consists of compressor, combustion chamber, and turbine sections. This type of engine works in the Brayton Cycle principle that is compression of atmospheric flow, combustion of air-fuel mixture and expanding high temperature combustion flow to generate power output from turbine. The aim of this study is to determine the duct geometry and flow conditions of the gas turbine blades having the internal cooling ducts that acquire highest heat transfer on turbine blades. For different design of internal duct geometries and flow conditions, Fluent solver i

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DASH, SUNIL MANOHAR, and THONG-SEE LEE. "IMPULSIVELY STARTED FLOW TOPOLOGY AROUND TANDEM ARRANGEMENT OF TWO SQUARE CYLINDER AT INCIDENCE." International Journal of Modern Physics: Conference Series 19 (January 2012): 100–108. http://dx.doi.org/10.1142/s201019451200863x.

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Numerical study of impulsively started flow over two tandem square cylinders where former cylinder is rotated at angles (0-45deg) to main stream flow direction keeping later one inline to flow stream with a separation of twice the side length of square prism between the centers of cylinders is performed using FVM code solver FLUENT 6.3.26. Temporal developments of streamlines around cylinders are studied for laminar flow regime ( Re = 100). Flow pattern formed are categories into Type-1, Type-2, Type-3 & Type-4 as per vortices growth at corresponding angle of incidence which are novel resu

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