Openfoam for Computational Fluid Dynamics
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Stall/Surge Dynamics of a Multi-Stage Air Compressor in Response to a Load Transient of a Hybrid Solid Oxide Fuel Cell-Gas Turbine System
Journal of Power Sources 365 (2017) 408e418 Contents lists available at ScienceDirect Journal of Power Sources journal homepage: www.elsevier.com/locate/jpowsour Stall/surge dynamics of a multi-stage air compressor in response to a load transient of a hybrid solid oxide fuel cell-gas turbine system * Mohammad Ali Azizi, Jacob Brouwer Advanced Power and Energy Program, University of California, Irvine, USA highlights Dynamic operation of a hybrid solid oxide fuel cell gas turbine system was explored. Computational fluid dynamic simulations of a multi-stage compressor were accomplished. Stall/surge dynamics in response to a pressure perturbation were evaluated. The multi-stage radial compressor was found robust to the pressure dynamics studied. Air flow was maintained positive without entering into severe deep surge conditions. article info abstract Article history: A better understanding of turbulent unsteady flows in gas turbine systems is necessary to design and Received 14 August 2017 control compressors for hybrid fuel cell-gas turbine systems. Compressor stall/surge analysis for a 4 MW Accepted 4 September 2017 hybrid solid oxide fuel cell-gas turbine system for locomotive applications is performed based upon a 1.7 MW multi-stage air compressor. Control strategies are applied to prevent operation of the hybrid SOFC-GT beyond the stall/surge lines of the compressor. Computational fluid dynamics tools are used to Keywords: simulate the flow distribution and instabilities near the stall/surge line. The results show that a 1.7 MW Solid oxide fuel cell system compressor like that of a Kawasaki gas turbine is an appropriate choice among the industrial Hybrid fuel cell gas turbine Dynamic simulation compressors to be used in a 4 MW locomotive SOFC-GT with topping cycle design. -
CFD Based Design for Ejector Cooling System Using HFOS (1234Ze(E) and 1234Yf)
energies Article CFD Based Design for Ejector Cooling System Using HFOS (1234ze(E) and 1234yf) Anas F A Elbarghthi 1,*, Saleh Mohamed 2, Van Vu Nguyen 1 and Vaclav Dvorak 1 1 Department of Applied Mechanics, Faculty of Mechanical Engineering, Technical University of Liberec, Studentská 1402/2, 46117 Liberec, Czech Republic; [email protected] (V.V.N.); [email protected] (V.D.) 2 Department of Mechanical and Materials Engineering, Masdar Institute, Khalifa University of Science and Technology, Abu Dhabi, UAE; [email protected] * Correspondence: [email protected] Received: 18 February 2020; Accepted: 14 March 2020; Published: 18 March 2020 Abstract: The field of computational fluid dynamics has been rekindled by recent researchers to unleash this powerful tool to predict the ejector design, as well as to analyse and improve its performance. In this paper, CFD simulation was conducted to model a 2-D axisymmetric supersonic ejector using NIST real gas model integrated in ANSYS Fluent to probe the physical insight and consistent with accurate solutions. HFOs (1234ze(E) and 1234yf) were used as working fluids for their promising alternatives, low global warming potential (GWP), and adhering to EU Council regulations. The impact of different operating conditions, performance maps, and the Pareto frontier performance approach were investigated. The expansion ratio of both refrigerants has been accomplished in linear relationship using their critical compression ratio within 0.30% accuracy. The results show that ± R1234yf achieved reasonably better overall performance than R1234ze(E). Generally, by increasing the primary flow inlet saturation temperature and pressure, the entrainment ratio will be lower, and this allows for a higher critical operating back pressure. -
Advanced Molecular Dynamics in Openfoam✩ S.M
Computer Physics Communications 224 (2018) 1–21 Contents lists available at ScienceDirect Computer Physics Communications journal homepage: www.elsevier.com/locate/cpc Feature article mdFoam+: Advanced molecular dynamics in OpenFOAMI S.M. Longshaw a,*, M.K. Borg b, S.B. Ramisetti b, J. Zhang b, D.A. Lockerby c, D.R. Emerson a, J.M. Reese b a Scientific Computing Department, The Science & Technology Facilities Council, Daresbury Laboratory, Warrington, Cheshire WA4 4AD, UK b School of Engineering, University of Edinburgh, Edinburgh EH9 3FB, UK c School of Engineering, University of Warwick, Coventry, CV4 7AL, UK article info a b s t r a c t Article history: This paper introduces mdFoam+, which is an MPI parallelised molecular dynamics (MD) solver imple- Received 6 March 2017 mented entirely within the OpenFOAM software framework. It is open-source and released under the Received in revised form 17 August 2017 same GNU General Public License (GPL) as OpenFOAM. The source code is released as a publicly open Accepted 25 September 2017 software repository that includes detailed documentation and tutorial cases. Since mdFoam+ is designed Available online 23 October 2017 entirely within the OpenFOAM C++ object-oriented framework, it inherits a number of key features. The Keywords: code is designed for extensibility and flexibility, so it is aimed first and foremost as an MD research tool, OpenFOAM in which new models and test cases can be developed and tested rapidly. Implementing mdFoam+ in Molecular dynamics OpenFOAM also enables easier development of hybrid methods that couple MD with continuum-based MD solvers. Setting up MD cases follows the standard OpenFOAM format, as mdFoam+ also relies upon Computational fluid dynamics the OpenFOAM dictionary-based directory structure. -
Introduction to Nuclear Reactor Modelling Using Openfoam Carlo Fiorina 2
Introduction to nuclear reactor modelling using OpenFOAM Carlo Fiorina 2 Disclaimer C. Fiorina ▪ Focus on the use of OpenFOAM for multiphysics ○ Use of OpenFOAM as CFD tool widely covered by documentation, forums, courses, etc. ▪ Focus on already existing tool (GeN-Foam) as an example ○ Programming from scratch is not that difficult, but unsuited for a 75 minutes lecture ▪ In the slides, more material than can actually be covered in this lecture ○ Can help better understanding the slides after the lecture 3 Content C. Fiorina ▪ General Introduction ▪ Introduction to the use of OpenFOAM ▪ Basics of GeN-Foam ▪ Short introduction on the use of GeN-Foam 4 Objective C. Fiorina What is it about? ▪ Provide you with general information, references, suggestions, terminology and lessons learnt that can facilitate your approach to the OpenFOAM world ▪ Provide with slides that can help you out orienting yourself if you decide to embrace the use of OpenFOAM What is not about? ▪ Detailed course on the use of OpenFOAM ▪ Hands-on training 5 The IAEA-facilitated ONCORE initiative C. Fiorina ONCORE to support the open-source nuclear community and help addressing typical shortcomings of open-source development (scattered community, documentation, QA, loss of knowledge) ▪ Promote collaboration and facilitate communication (connect the community) ▪ Provide guidelines for code contribution (documentation, QA) ▪ Provide development best practices (QA) ▪ Preserve knowledge ○ Incl. compiling a list of open-source codes https://www.iaea.org/topics/nuclear-power-reactors/open-source-nuclear-cod e-for-reactor-analysis-oncore 6 A first important outcome: list of C. Fiorina available codes ▪ https://nucleus.iaea.org/sites/oncore/SitePages/List%20of%20Codes.aspx ▪ A vibrant community with an impressive R&D output ▪ ~35 codes already identified so far: ○ OpenMC ○ Raven ○ Dragon ○ MOOSE ○ Salome platform (Code_Saturne, Code_Aster) ○ TrioCFD ○ … ○ Several OpenFOAM-based tools 7 A central tool for open-source simulation C. -
MSME with Depth in Fluid Mechanics
MSME with depth in Fluid Mechanics The primary areas of fluid mechanics research at Michigan State University's Mechanical Engineering program are in developing computational methods for the prediction of complex flows, in devising experimental methods of measurement, and in applying them to improve understanding of fluid-flow phenomena. Theoretical fluid dynamics courses provide a foundation for this research as well as for related studies in areas such as combustion, heat transfer, thermal power engineering, materials processing, bioengineering and in aspects of manufacturing engineering. MS Track for Fluid Mechanics The MSME degree program for fluid mechanics is based around two graduate-level foundation courses offered through the Department of Mechanical Engineering (ME). These courses are ME 830 Fluid Mechanics I Fall ME 840 Computational Fluid Mechanics and Heat Transfer Spring The ME 830 course is the basic graduate level course in the continuum theory of fluid mechanics that all students should take. In the ME 840 course, the theoretical understanding gained in ME 830 is supplemented with material on numerical methods, discretization of equations, and stability constraints appropriate for developing and using computational methods of solution to fluid mechanics and convective heat transfer problems. Students augment these courses with additional courses in fluid mechanics and satisfy breadth requirements by selecting courses in the areas of Thermal Sciences, Mechanical and Dynamical Systems, and Solid and Structural Mechanics. Graduate Course and Research Topics (Profs. Benard, Brereton, Jaberi, Koochesfahani, Naguib) ExperimentalResearch Many fluid flow phenomena are too complicated to be understood fully or predicted accurately by either theory or computational methods. Sometimes the boundary conditions of real-world problems cannot be analyzed accurately. -
15Th Openfoam Workshop - June 22, 2020 - Technical Session I-D a Flexible and Precice Solver Coupling Ecosystem
15th OpenFOAM Workshop - June 22, 2020 - Technical Session I-D A flexible and preCICE solver coupling ecosystem Gerasimos Chourdakis, Technical University of Munich [email protected] Benjamin Uekermann, Eindhoven University of Technology [email protected] Find these slides on GitHub https://github.com/MakisH/ofw15-slides The Big Picture e r ic r te c e p e lv a r o d p s a lib structure fluid solver solver The Big Picture e r ic r te c e p e lv a r o d p s a lib structure fluid solver solver in-house commercial solver solver The Big Picture e r ic r te c e p e lv a r o d p s a lib structure fluid solver solver OpenFOAM CalculiX SU2 Code_Aster foam-extend FEniCS deal-ii Nutils MBDyn in-house commercial solver solver API in: C++ Python Matlab ANSYS Fluent C Fortran COMSOL The Big Picture e r ic r te c e p e lv a r o d p s a lib structure fluid solver A Coupling Library for Partitioned Multi-Physics Simulations solver OpenFOAM CalculiX SU2 Code_Aster . foam-extend FEniCS deal-ii . Nutils MBDyn communication data mapping in-house commercial solver solver coupling schemes time interpolation API in: C++ Python Matlab ANSYS Fluent C Fortran COMSOL News preCICE v2.0 Simplified config & API Better building & testing XML reference & visualizer xSDK member Faster initialization Better Python bindings Spack / Debian / AUR New Matlab bindings packages Upgrade guide in the wiki Other news deal.ii adapter new non-linear example for FSI FEniCS adapter new example for FSI code_aster adapter revived for code_aster 14 and preCICE v2 The OpenFOAM adapter -
Model Order Reduction for Aerodynamic Lifting Surfaces Aerospace Engineering
Model Order Reduction for Aerodynamic Lifting Surfaces Gonçalo da Cunha Laboreiro Mendonça Thesis to obtain the Master of Science Degree in Aerospace Engineering Supervisors: Prof. Fernando José Parracho Lau Dr. Frederico José Prata Rente Reis Afonso Examination Committee Chairperson: Prof. Filipe Szolnoky Ramos Pinto Cunha Supervisor: Prof. Fernando José Parracho Lau Member of the Committee: Prof. Afzal Suleman November 2017 ii Dedicated to my family and friends, who were always there for me. iii iv Acknowledgments I would like to thank dearly my supervisors Prof. Lau and Dr. Afonso who gave me constant support throughout this thesis up until the very end. Their insights on aerodynamics and CFD models guided me in my research of model order reduction methods and allowed me to better understand the models with which I had to work. Their demands for rigor and quality also pushed me to better my work, and in the end write a better thesis. v vi Resumo Nesta tese o tema de reduc¸ao˜ de modelos e a sua aplicac¸ao˜ a Mecanicaˆ de Fluidos Computacional sao˜ abordados. E´ mostrada a necessidade da industria´ aeroespacial, seja nacional ou Europeia, de modelos mais rapidos´ mas fieis´ a` realidade. Isto e´ devido ao elevado tempo de calculo´ associado aos modelos de alta-fidelidade. Estes mostram-se pouco viaveis´ para aplicac¸oes˜ do tipo Optimizac¸ao˜ Multi- disciplinar, como a plataforma de optimizac¸ao˜ NOVEMOR. Tendo por objectivo testar e aplicar reduc¸ao˜ de modelos a modelos CFD de superf´ıcies sustentadoras, uma pesquisa bibliografica´ abrangendo a reduc¸ao˜ de modelos nao-lineares,˜ dinamicosˆ e ou estaticos´ foi feita. -
The One-Way FSI Method Based on RANS-FEM for the Open Water Test of a Marine Propeller at the Different Loading Conditions
Journal of Marine Science and Engineering Article The One-Way FSI Method Based on RANS-FEM for the Open Water Test of a Marine Propeller at the Different Loading Conditions Mobin Masoomi 1 and Amir Mosavi 2,3,* 1 Department of Mechanical Engineering, Babol Noshirvani University of Technology, Babol, Iran; [email protected] 2 Faculty of Civil Engineering, Technische Universität Dresden, 01069 Dresden, Germany 3 John von Neumann Faculty of Informatics, Obuda University, 1034 Budapest, Hungary * Correspondence: [email protected] Abstract: This paper aims to assess a new fluid–structure interaction (FSI) coupling approach for the vp1304 propeller to predict pressure and stress distributions with a low-cost and high-precision approach with the ability of repeatability for the number of different structural sets involved, other materials, or layup methods. An outline of the present coupling approach is based on an open- access software (OpenFOAM) as a fluid solver, and Abaqus used to evaluate and predict the blade’s deformation and strength in dry condition mode, which means the added mass effects due to propeller blades vibration is neglected. Wherein the imposed pressures on the blade surfaces are extracted for all time-steps. Then, these pressures are transferred to the structural solver as a load condition. Although this coupling approach was verified formerly (wedge impact), for the case in-hand, a further verification case, open water test, was performed to evaluate the hydrodynamic part of the solution with an e = 7.5% average error. A key factor for the current coupling approach is Citation: Masoomi, M.; Mosavi, A. -
Wind Field Simulation in a Wind Farm Using Openfoam and Actuator Line Model
ParCFD'2019 31st International Conference on Parallel Computational Fluid Dynamics May-14-17 2019, Antalya TURKEY WIND FIELD SIMULATION IN A WIND FARM USING OPENFOAM AND ACTUATOR LINE MODEL Huseyin Can Onel∗ & Dr. Ismail H. Tuncery ∗ Middle East Technical University (METU) Department of Aerospace Engineering 06800 Ankara, TURKEY e-mail: [email protected] yMiddle East Technical University (METU) Department of Aerospace Engineering 06800 Ankara, TURKEY e-mail: [email protected] - Web page: http://www.ae.metu.edu.tr/tuncer/ Key words: Aerospace applications, Wind turbine, HAWT, Actuator Line Model, Wake calculation Abstract. In this study, a horizontal axis wind turbine (HAWT) is modeled using so called Actuator Line Model (ALM), where full resolution of boundary layer over turbine blades is not needed and hence computation is cheaper. Results are validated against other numerical and experimental studies as well as panel method (XFOIL) and Blade Element Momentum Theory (BEMT) results which are still widely employed in today's wind energy industry. Important simulation and operation parameters and their effects on accuracy are discussed. It is concluded that within a certain range of tip speed ratios, ALM gives acceptable results and is a promising model for full-scale wind farm simulations to estimate energy production. 1 INTRODUCTION Market share of renewable energy grows at ever highest rates and wind turbine and wind farm design processes becomes more sophisticated with the advancements in computation technologies. There are two main design problems in wind energy: • Design of an individual wind turbine at its ideal operation conditions, where classical methods like 2D airfoil theory, potential flow theory and Blade Element Momentum Theory (BEMT) are still widely used, • Design of a complete wind farm, in which statistical meteorological data is used for macro-siting and simple analytical or empirical methods are used for micro-siting. -
COMSOL Computational Fluid Dynamics for Microreactors Used in Volatile Organic Compounds Catalytic Elimination
COMSOL Computational Fluid Dynamics for Microreactors Used in Volatile Organic Compounds Catalytic Elimination Maria Olea 1, S. Odiba1, S. Hodgson1, A. Adgar1 1School of Science and Engineering, Teesside University, Middlesbrough, United Kingdom Abstract Volatile organic compounds (VOCs) are organic chemicals that will evaporate easily into the air at room temperature and contribute majorly to the formation of photochemical ozone. They are emitted as gases from certain solids and liquids in to the atmosphere and affect indoor and outdoor air quality. They includes acetone, benzene, ethylene glycol, formaldehyde, methylene chloride, perchloroethylene, toluene, xylene, 1,3-butadiene, butane, pentane, propane, ethanol, etc. Source of VOCs emission include paints, industrial processes, transportation activities, household products such as cleaning agents, aerosols, fuel and cosmetics. Catalytic oxidation is one of the most promising elimination techniques for VOCs as a result of it flexibility and energy saving. The catalytic materials enhance the chemical reactions that convert VOCs (through oxidation) into carbon dioxide and water. Removal of volatile organic compounds at room temperature has always been a challenge to researchers. Developing a catalyst which could completely oxidize the VOCs at very low temperature in order to avoid catalyst deactivation and promote energy saving has been the key focus among researchers in the recent years. Moreover, as the oxidation reaction is highly exothermic, the use of catalytic microreactors instead of packed bed reactors was considered. Microreactors are microfabricated catalytic chemical reactors with at least one linear dimension in the micrometer range. Usually, they consist of narrow channels and exhibit large surface area-to- volume ratios which leads to high heat and mass transfer properties. -
THERMODYNAMICS, HEAT TRANSFER, and FLUID FLOW, Module 3 Fluid Flow Blank Fluid Flow TABLE of CONTENTS
Department of Energy Fundamentals Handbook THERMODYNAMICS, HEAT TRANSFER, AND FLUID FLOW, Module 3 Fluid Flow blank Fluid Flow TABLE OF CONTENTS TABLE OF CONTENTS LIST OF FIGURES .................................................. iv LIST OF TABLES ................................................... v REFERENCES ..................................................... vi OBJECTIVES ..................................................... vii CONTINUITY EQUATION ............................................ 1 Introduction .................................................. 1 Properties of Fluids ............................................. 2 Buoyancy .................................................... 2 Compressibility ................................................ 3 Relationship Between Depth and Pressure ............................. 3 Pascal’s Law .................................................. 7 Control Volume ............................................... 8 Volumetric Flow Rate ........................................... 9 Mass Flow Rate ............................................... 9 Conservation of Mass ........................................... 10 Steady-State Flow ............................................. 10 Continuity Equation ............................................ 11 Summary ................................................... 16 LAMINAR AND TURBULENT FLOW ................................... 17 Flow Regimes ................................................ 17 Laminar Flow ............................................... -
Performance Evaluation of Multipurpose Solar Heating System
Mechanics and Mechanical Engineering Vol. 20, No. 4 (2016) 359{370 ⃝c Lodz University of Technology Performance Evaluation of Multipurpose Solar Heating System R. Venkatesh Department of Mechanical Engineering Srinivasan Engineering College Perambalur, Tamilnadu, India V. Vijayan Department of Mechanical Engineering K. Ramakrishnan College of Technology Samayapuram, Trichy, Tamilnadu, India Received (29 May 2016) Revised (26 July 2016) Accepted (25 September 2016) In order to increase the heat transfer and thermal performance of solar collectors, a multipurpose solar collector is designed and investigated experimentally by combining the solar water collector and solar air collector. In this design, the storage tank of the conventional solar water collector is modified as riser tubes and header and is fitted in the bottom of the solar air heater. This paper presents the study of fluid flow and heat transfer in a multipurpose solar air heater by using Computational Fluid Dynamics (CFD) which reduces time and cost. The result reveals that in the multipurpose solar air heater at load condition, for flow rate of 0.0176 m3/s m2, the maximum average thermal efficiency was 73.06% for summer and 67.15 % for winter season. In multipurpose solar air heating system, the simulated results are compared to experimental values and the deviation falls within ± 11.61% for summer season and ± 10.64% for winter season. It proves that the simulated (CFD) results falls within the acceptable limits. Keywords: solar water collector, solar air collector, fluid flow, heat transfer and Compu- tational fluid dynamics. 1. Introduction Solar energy plays an important role in low{temperature thermal applications, since it replaces a considerable amount of conventional fuel.