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Academic literature on the topic 'CFD analysis'

Author: Grafiati

Published: 4 June 2021

Last updated: 11 September 2023

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Journal articles on the topic "CFD analysis"

1

CHO, SU K., and VAMSHI M. KORIVI. "PORT DESIGN OPTIMIZATION USING CFD ANALYSIS." Journal of Advanced Manufacturing Systems 03, no. 01 (June 2004): 21–32. http://dx.doi.org/10.1142/s0219686704000375.

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Shape of ports that are part of an engine cylinder head is vital to engine performance and emissions. The advance of CFD (Computation Fluid Dynamics) analysis technology helps designers run the simulation to improve the port design and to provide the better model for a flow bench test. This paper presents the automation of design optimization process integrating CAD modeling, mesh generation and CFD simulation.

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Scheer, Justin K., Jessica Tang, Johnny Eguizabal, Azadeh Farin, Jenni M. Buckley, Vedat Deviren, R. Trigg McClellan, and Christopher P. Ames. "Optimal reconstruction technique after C-2 corpectomy and spondylectomy: a biomechanical analysis." Journal of Neurosurgery: Spine 12, no. 5 (May 2010): 517–24. http://dx.doi.org/10.3171/2009.11.spine09480.

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Object Primary spine tumors frequently involve the C-2 vertebra. Complete resection of the lesion may require total removal of the C-2 vertebral body, pedicles, and dens process. Authors of this biomechanical study are the first to evaluate a comprehensive set of reconstruction methods after C-2 resection to determine the optimal configuration depending on the degree of excision required. Methods Eight human heads (from the skull to C-6) from 4 males and 4 females with a mean age of 68 ± 18 years at death were cleaned of tissue, while leaving ligaments and discs intact. Nondestructive flexion and extension (FE), lateral bending (LB), and axial rotation (AR) tests were conducted using a nonconstraining, pure moment loading apparatus, and relative motion across the fusion site (C1–3) was measured using a 3D motion tracking system. Specimens were tested up to 1.5 Nm at 0.25-Nm intervals for 45 seconds each. The spines were instrumented using 3.5-mm titanium rods with a midline occipitocervical plate (4.0 × 12–mm screws) and lateral mass screws (excluding C-2) at the C-1 (3.0 × 40 mm) and C3–5 levels (3.0 × 16 mm). Testing was repeated for the following configurations: Configuration 1 (CF1), instrumentation only from occiput to C-5; CF2, C-2 corpectomy leaving the dens; CF3, titanium mesh cage (16-mm diameter) from C-3 to C-1 ring and dens; CF4, removal of cage, C-1 ring, and dens; CF5, titanium mesh cage from C-3 to clivus (16-mm diameter); CF6, removal of C-2 posterior elements leaving the C3–clivus cage (spondylectomy); CF7, titanium mesh cage from C-3 to clivus (16-mm diameter) with 2 titanium mesh cages from C-3 to C-1 lateral masses (12-mm diameter); and CF8, removal of all 3 cages. A crosslink was added connecting the posterior rods for CF1, CF6, and CF8. Range-of-motion (ROM) differences between all groups were compared via repeated-measures ANOVA with paired comparisons using the Student t-test with a Tukey post hoc adjustment. A p < 0.05 indicated significance. Results The addition of a central cage significantly increased FE rigidity compared with posterior instrumentation alone but had less of an effect in AR and LB. The addition of lateral cages did not significantly improve rigidity in any bending direction (CF6 vs CF7, p > 0.05). With posterior instrumentation alone (CF1 and CF2), C-2 corpectomy reduced bending rigidity in only the FE direction (p < 0.05). The removal of C-2 posterior elements in the presence of a C3–clivus cage did not affect the ROM in any bending mode (CF5 vs CF6, p > 0.05). A crosslink addition in CF1, CF6, and CF8 did not significantly affect primary or off-axis ROM (p > 0.05). Conclusions Study results indicated that posterior instrumentation alone with 3.5-mm rods is insufficient for stability restoration after a C-2 corpectomy. Either C3–1 or C3–clivus cages can correct instability introduced by C-2 removal in the presence of posterior instrumentation. The addition of lateral cages to a C3–clivus fusion construct may be unnecessary since it does not significantly improve rigidity in any direction.

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Patel, Karna S., Saumil B. Patel, Utsav B. Patel, and Prof Ankit P. Ahuja. "CFD Analysis of an Aerofoil." International Journal of Engineering Research 3, no. 3 (March 1, 2014): 154–58. http://dx.doi.org/10.17950/ijer/v3s3/305.

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Thilmany, Jean. "In-School Analysis." Mechanical Engineering 130, no. 01 (January 1, 2008): 32–35. http://dx.doi.org/10.1115/1.2008-jan-3.

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This article highlights introducing undergrads to computerized fluid dynamics (CFD) and FEA software that is not a straightforward affair. Computerized fluid dynamics has become mainstream more recently, but many engineers are finding it just as important to their daily work. In order to prepare engineers to enter such a world, professors have begun a conversation to determine the best way and the best time to introduce students to the analysis software they will likely need on the job. The subject is more challenging, both to learn and to introduce into the curriculum, than computer-aided design. Instructors agree that their students first need a good grounding in CAD before moving on to analysis. Introduction to the software comes after instructors are sure students are comfortable with CAD and have become familiar with a range of analysis concepts. Teaching CAD is a lot easier than teaching CAE, so schools are finding they cannot substitute their CAD teaching methods when it comes to CFD and FEA.

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Pieritz, R. A., R. Mendes, R. Ferraz, and C. R. Maliska. "CFD STUDIO: AN EDUCATIONAL SOFTWARE FOR CFD ANALYSIS." Revista de Engenharia Térmica 2, no. 2 (December 31, 2003): 09. http://dx.doi.org/10.5380/reterm.v2i2.3471.

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The main goal of this paper is to demonstrate the general characteristics of the educational user-friendly CFD Studio package for CFD teaching. The package was designed for teaching 2D fluid mechanics and heat transfer process, including conduction, coupled conduction/convection, natural and forced convection, external and internal flows, among other phenomena. The finite volume methodology and its related topics can also be taught using the software. Therefore, general aspects of the three main modules, pre-processor, solver and post-processor are discussed aiming to show the generality of the tool. These modules are integrated in the application by a so-called numerical problem project which guide the student through the steps to obtain the solution. To approximate the partial differential equations the finite volume approach is employed using a fully-implicit formulation with the interpolation schemes CDS, UDS and WUDS. Mesh editing and nonorthogonal boundary-fitted mesh generation, using algebraic interpolation and elliptic equations, are important features of the package. Coupled heat transfer problems are handled using the solid-block formulation and the pressure-velocity coupling uses the SIMPLE and SIMPLEC methods with non-staggered grids. To demonstrate the capabilities two fluid flow and heat transfer problem projects are presented.

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Lin, Chen-Jiann, Tseng-Hsiang Tse, Liu-Cheng Che, and Liang-Ming Tsai. "Computer aided design and analysis on distributors in DAC columns." MATEC Web of Conferences 185 (2018): 00024. http://dx.doi.org/10.1051/matecconf/201818500024.

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Dynamic axial compression (DAC) columns are key elements in simulated moving bed, which is a chromatography process in drug industry and chemical engineering. In this study, rules for designing distributors are proposed based on mass conservation and validated by experiments, the computer aided design (CAD) and the computational fluid dynamics (CFD). Experimental works are conducted to choose feasible numerical parameters for simulations. In CFD, the transient laminar flow fields are governed by the momentum and species transport equations with Darcy's law to model the porous zone in the packed bed. Results show that CFD combined with CAD solid modelling is a good approach to explore detailed flow fields in DAC columns and carry out parameter analysis for innovative designs. For further testing and evaluation, a new model of compound distributor is designed, 3D printed and processed in factory for practical applications in preparative chromatography.

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Gao, Yan, and Songlin Liu. "Higher-Order Compact Finite Difference for Certain PDEs in Arbitrary Dimensions." Journal of Function Spaces 2020 (November 24, 2020): 1–12. http://dx.doi.org/10.1155/2020/8567605.

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In this paper, we first present the expression of a model of a fourth-order compact finite difference (CFD) scheme for the convection diffusion equation with variable convection coefficient. Then, we also obtain the fourth-order CFD schemes of the diffusion equation with variable diffusion coefficients. In addition, a fine description of the sixth-order CFD schemes is also developed for equations with constant coefficients, which is used to discuss certain partial differential equations (PDEs) with arbitrary dimensions. In this paper, various ways of numerical test calculations are prepared to evaluate performance of the fourth-order CFD and sixth-order CFD schemes, respectively, and the empirical results are proved to verify the effectiveness of the schemes in this paper.

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Krishnara J, C., S. Rajesh Ruban, and N. Subramani. "Analysis of exhaust manifold to improve the engine performance." International Journal of Engineering & Technology 7, no. 2.8 (March 19, 2018): 539. http://dx.doi.org/10.14419/ijet.v7i2.8.10517.

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The aim of the work is to analyze the performance of the engine exhaust manifold. Because the engine exhaust manifold is a significant factor in the engine performance. In this work the manifold design is prepared with the help of CAD software and it is analyzed by the ANSYS. This CFD and thermal analysis also done to check the performance of the redesigned exhaust manifold. The aim of CFD simulations performed to investigate the volumetric efficiency behaviour of an exhaust.

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Spanu, Simone, David Mosna, and Giuseppe Vignali. "CFD Analysis of Coffee Packaging in Capsules using Gas Flushing Modified Atmosphere Packaging." International Journal of Food Engineering 12, no. 9 (November 1, 2016): 875–87. http://dx.doi.org/10.1515/ijfe-2016-0047.

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Abstract The aim of this work is to analyze, by means of CFD (Computational Fluid Dynamics), the gas flow in a packaging machine used to fill polymeric capsules with coffee. The final goal is to optimize the geometric shape of some mechanical components in the machine’s sealing station in order to reduce the inert gas consumption achieving an O2 residual which is constantly equal or below 1 % by mass in the center of the capsule. The fluid domain has been obtained starting from the 3D CAD model of the sealing station of the packaging machine. The CAD software SolidWorks has been used to design the system, while Ansys CFX 14.5 software has been used for the CFD analysis. The CFD model has been validated by comparing its results with those obtained by experimental tests. The modified solution allows reducing the average O2 residual from about 3 % to less than 1 %.

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King, Matthew L., Matthew J. Fisher, and C. Greg Jensen. "A CAD-centric Approach to CFD Analysis With Discrete Features." Computer-Aided Design and Applications 3, no. 1-4 (January 2006): 279–88. http://dx.doi.org/10.1080/16864360.2006.10738465.

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Dissertations / Theses on the topic "CFD analysis"

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King, Matthew Lee. "A CAD-centric Approach to CFD Analysis With Discrete Features." Diss., CLICK HERE for online access, 2004. http://contentdm.lib.byu.edu/ETD/image/etd570.pdf.

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Barstad, Lorentz Fjellanger. "CFD Analysis of a Pelton Turbine." Thesis, Norges teknisk-naturvitenskapelige universitet, Institutt for energi- og prosessteknikk, 2012. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-18598.

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A Pelton design software is currently being developed at the Waterpower laboratory at NTNU. The motivation behind this software is to streamline the parametric design process for Pelton turbines. A numerical flow model is a cornerstone in this application, but the lack of a bucket geometry and model runner has prevented the development of such a model. DynaVec, a turbine producer who specializes on sediment erosion and corrosion problems, offered to help by providing a bucket geometry and a model runner.The objective of this Master's thesis was to develop and validate a CFD model that predicts the torque applied to a non-stationary Pelton bucket, subject to a high-speed water jet. The numerical model was based on a method proposed by DynaVec, and the bucket geometry used in the simulations was identical (1:1) to the model runner.Numerous simulations were conducted, testing mesh dependency and different operational points (e.g. head). Mesh independence occurred at approximately 4.5 million elements. Furthermore, simulations of varying heads showed that the model may be independent of the head (40-80m), but this was not verified properly.Experiments showed that the numerical prediction was fairly accurate. A comparison of the numerical and experimental measurements showed that the CFD model over-predicts the torque by approximately 1.5%. This prediction was validated for the specific geometry used in the simulations, and a head of 75m.Overall, the results suggest that the numerical model is promising as a parametric design tool, but further development is required to obtain a true validation of the model.Task three and four were changed in agreement with Ole Gunnar Dahlhaug, because Solemslie's design program was delayed. In essence, the parametric study proceeded in favor of the development of a CFD model. To ensure that this work would benefit future research, especially students at the Waterpower laboratory, a detailed procedure for the CAD modeling, meshing and physical setup was included in the Appendix.

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Thelin, Fredrik. "A CFD Analysis of Cyclodial Propellers." Thesis, Linköpings universitet, Mekanisk värmeteori och strömningslära, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:liu:diva-144535.

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The quest for more efficient machines is always ongoing in the engineering world. This project is no different. ABB are investigating a new type of propeller that seems to offer increased efficiency compared to normal screw propellers. That is a so called foil wheel propeller. The foil move in a circular pattern with the fluid stream moving in the radial direction of the propeller instead of the axial as in a screw propeller. If the propeller is placed and modeled correctly it can also be used as a thrust vectoring device. This report focuses on the fluid physics of the foil wheel propeller, or as it is called in this report radial flow propeller. First of all the movements and interactions of the blades must be understood. Both to keep the efficiency high to compete with screw propellers, but also to foresee any problems that may occur with such a new device. A scaled down version of the propeller have been commissioned by ABB and will be tested in some time after the work within this report is completed. The effects associated to this will also be analyzed. The tool to compute the flow physics of the radial flow propeller will be computational fluid dynamics. Computational fluid dynamics uses a numerical method to compute the entire fluid field in space and time. The flow around the propeller is highly complex so a detailed analysis is needed if a well functioning control system is to be constructed for instance. The differences between the downscale and the full-scale are great, even when the non dimensional coefficients are considered. The down-scale case will be less efficient, it will be difficulties predicting the performance of the full-scale since the downscale flow is much less powerful than the full-scale case. The interaction between the blades has a large effect. There is a strong relation between angle of attack and the number of blades. The forces that are large change by about 30\% so it must definitely be considered if a model is to be used for a control system.

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Juretic, Franjo. "Error analysis in finite volume CFD." Thesis, Imperial College London, 2005. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.420616.

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Spentzos, Agis. "CFD analysis of 3D dynamic stall." Thesis, University of Glasgow, 2005. http://theses.gla.ac.uk/1855/.

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Focusing on helicopter aerodynamics, it is known that the aerodynamic performance of the retreating side of a rotor disk is mainly dictated by the stall characteristics of the blade. Stall under dynamic conditions (Dynamic Stall) is the dominant phenomenon encountered on heavily loaded fast-flying rotors, resulting in an extra lift and excessive pitching moments. Dynamic stall (DS) can be idealised as the pitching motion of a finite wing and this is the focus of the present work which includes three main stages. At first, comparisons between available experimental data with CFD simulations were performed for 3D DS cases. This work is the first detailed CFD study of 3D Dynamic Stall and has produced results indicating that DS can be predicted and analysed using CFD. The CFD results were validated against all known experimental investigations. In addition, a comprehensive set of CFD results was generated and used to enhance our understanding of 3D DS. Straight, tapered and swept-tip wings of various aspect ratios were used at a range of Reynolds and Mach numbers and flow conditions. For all cases where experimental data were available effort was put to obtain the original data and process these in exactly the same ways as the CFD results. Special care was put to represent exactly the motion of the lifting surfaces, its geometry and the boundary conditions of the problem. Secondly, the evolution of the Ω-shaped DS vortex observed in experimental works as well as its interaction with the tip vortices were investigated. Both pitching and pitching/rotating blade conditions were considered. Finally, the potential of training a Neural network as a model for DS was assessed in an attempt to reduce the required CPU time for modelling 3D DS. Neural networks have a proven track record in applications involving pattern recognition but so far have seen little application in unsteady aerodynamics. In this work, two different NN models were developed and assessed in a variety of conditions involving DS. Both experimental and CFD data were used during these investigations. The dependence of the quality of the predictions of the NN on the choice of the training data was then assessed and thoughts towards the correct strategy behind this choice were laid out.

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Kokkonen, Toni. "CFD analysis of stepped planing vessels." Thesis, KTH, Mekanik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-250023.

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

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Ghate, Devendra. "Inexpensive uncertainty analysis for CFD applications." Thesis, University of Oxford, 2014. http://ora.ox.ac.uk/objects/uuid:6be44a1d-6e2f-4bf9-b1e5-1468f92e21e3.

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The work presented in this thesis aims to provide various tools to be used during design process to make maximum use of the increasing availability of accurate engine blade measurement data for high fidelity fluid mechanic simulations at a reasonable computational expense. A new method for uncertainty propagation for geometric error has been proposed for fluid mechanics codes using adjoint error correction. Inexpensive Monte Carlo (IMC) method targets small uncertainties and provides complete probability distribution for the objective function at a significantly reduced computational cost. A brief literature survey of the existing methods is followed by the formulation of IMC. An example algebraic model is used to demonstrate the IMC method. The IMC method is extended to fluid mechanic applications using Principal Component Analysis (PCA) for reduced order modelling. Implementation details for the IMC method are discussed using an example airfoil code. Finally, the IMC method has been implemented and validated for an industrial fluid mechanic code HYDRA. A consistent methodology has been developed for the automatic generation of the linear and adjoint codes by selective use of automatic differentiation (AD) technique. The method has the advantage of keeping the linear and the adjoint codes in-sync with the changes in the underlying nonlinear fluid mechanic solver. The use of various consistency checks have been demonstrated to ease the development and maintenance process of the linear and the adjoint codes. The use of AD has been extended for the calculation of the complete Hessian using forward-on-forward approach. The complete mathematical formulation for Hessian calculation using the linear and the adjoint solutions has been outlined for fluid mechanic solvers. An efficient implementation for the Hessian calculation is demonstrated using the airfoil code. A new application of the Independent Component Analysis (ICA) is proposed for manufacturing uncertainty source identification. The mathematical formulation is outlined followed by an example application of ICA for artificially generated uncertainty for the NACA0012 airfoil.

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Kern, Simon. "Sensitivity Analysis in 3D Turbine CFD." Thesis, KTH, Mekanik, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-210821.

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A better understanding of turbine performance and its sensitivity to variations in the inletboundary conditions is crucial in the quest of further improving the efficiency of aero engines.Within the research efforts to reach this goal, a high-pressure turbine test rig has been designedby Rolls-Royce Deutschland in cooperation with the Deutsches Zentrum für Luft- und Raumfahrt(DLR), the German Aerospace Center. The scope of the test rig is high-precision measurement ofaerodynamic efficiency including the effects of film cooling and secondary air flows as well as theimprovement of numerical prediction tools, especially 3D Computational Fluid Dynamics (CFD).A sensitivity analysis of the test rig based on detailed 3D CFD computations was carried outwith the aim to quantify the influence of inlet boundary condition variations occurring in the testrig on the outlet capacity of the first stage nozzle guide vane (NGV) and the turbine efficiency.The analysis considered variations of the cooling and rimseal leakage mass flow rates as well asfluctuations in the inlet distributions of total temperature and pressure. The influence of anincreased rotor tip clearance was also studied.This thesis covers the creation, calibration and validation of the steady state 3D CFD modelof the full turbine domain. All relevant geometrical details of the blades, walls and the rimsealcavities are included with the exception of the film cooling holes that are replaced by a volumesource term based cooling strip model to reduce the computational cost of the analysis. Thehigh-fidelity CFD computation is run only on a sample of parameter combinations spread overthe entire input parameter space determined using the optimal latin hypercube technique. Thesubsequent sensitivity analysis is based on a Kriging response surface model fit to the sampledata. The results are discussed with regard to the planned experimental campaign on the test rigand general conclusions concerning the impacts of the studied parameters on turbine performanceare deduced.

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URBANO, DARIO GIUSEPPE. "CFD ANALYSIS OF A VACUUM MICROGRIPPER." Doctoral thesis, Università degli studi di Brescia, 2021. http://hdl.handle.net/11379/550301.

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Aljure, Osorio David Eduardo. "Aerodynamic analysis of complex geometries using CFD." Doctoral thesis, Universitat Politècnica de Catalunya, 2017. http://hdl.handle.net/10803/454977.

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Aerodynamic analysis has become one of the most important tools in many engineering applications. In this sense, this thesis work is aimed at performing aerodynamic analysis of different geometries, expanding the available knowledge and obtaining valuable insight from the obtained results. Aerodynamic analysis can be carried out, principally, in two ways: Experimental research and Computational Fluid Dynamics (CFD). The former makes use of prototypes, wind tunnels and test tracks, making it a very expensive option. On the other hand, CFD makes use of numerical tools to solve the Navier-Stokes equations within a computational discretized domain. This latter approach is essentially limited by the available computational power and by the aerodynamicist's experience. This work comprises eight chapters. The first one is an introduction to the type of flows and geometries considered, as well as, the general methodology followed in the posterior studies. The following six chapters are the core of this dissertation, and encompass the numerical resolution of the Navier-Stokes equations in selected geometries, ordered by complexity level. In particular, the contents of these seven chapters have been submitted or published in international journals and conferences. For this reason, they are self contained and few changes have been made. The reader might find that some concepts are repeated along them. The last chapter contains concluding remarks. Finally, appendix 1 describes some applications of aerodynamic studies to some related projects and appendix 2 comprises a list of publications done during the PhD.
El análisis aerodinámico se ha convertido en una de las herramientas más importantes en diversidad de aplicaciones de ingeniería. En este contexto, esta tesis está enfocada a realizar análisis aerodinámicos en diferentes geometrías, contribuyendo datos nuevos a la comunidad científica y extrayendo información útil de los resultados obtenidos. Dichos análisis se pueden realizar, principalmente, de dos maneras: Mediante investigación experimental y mediante simulaciones numéricas (CFD). Para realizar experimentos se han de construir prototipos para su uso en túneles de viento y pistas de prueba, con los altos costos que esto conlleva. En otro extremo se encuentra el CFD, donde haciendo uso de herramientas computacionales se resuelven numéricamente las ecuaciones de Navier-Stokes en un dominio computacional. Este segundo enfoque se ve limitado por la potencia de cálculo disponible y la experiencia del aerodinamicista. Este trabajo se compone de ocho capítulos. En el primer capítulo se realiza una breve introducción a los tipos de flujos y geometrías consideradas en este estudio, así como la metodología a usar en el resto de capítulos . Los siguientes seis capítulos constituyen el cuerpo de este documento, y presentan la solución numérica y posterior análisis de las ecuaciones de Navier-Stokes en algunas geometrías de relevancia. Los contenidos de estos seis capítulos han sido presentados para su publicación en revistas indexadas y congresos. El último capítulo presenta las conclusiones extraídas de la presente tesis. Finalmente, el apéndice 1 presenta el análisis aerodinámico aplicado a problemas industriales reales, mientras que el apéndice 2 presenta la lista de publicaciones realizadas durante el desarrollo del doctorado.

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Books on the topic "CFD analysis"

1

A grassroots campaign for CFD analysis. [New York, N.Y.]: Knovel, 2010.

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Mather A. R. Sadiq Al-Baghdadi. CFD models for analysis and design of PEM fuel cells CFD models for analysis & design of PEM fuel cells. New York: Nova Science Publishers, 2008.

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United States. National Aeronautics and Space Administration., ed. CFD methods development considerations for unsteady aerodynamic analysis. [Washington, DC]: National Aeronautics and Space Administration, 1992.

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Luigi, Martinelli, and Research Institute for Advanced Computer Science (U.S.), eds. CFD analysis and design optimization using parallel computers. [Moffett Field, Calif.]: Research Institute for Advanced Computer Science, NASA Ames Research Center, 1997.

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Conference of the CFD Society of Canada (2nd 1994 Toronto, Ont.). CFD 94: Second Annual Conference of the CFD Society of Canada : proceedings = Deuxième congrès annuel de la société canadienne de CFD : comptes rendus : Toronto, Ontario, June 1-3, 1994. Edited by Gottlieb James J, Ethier C. Ross, and Computational Fluid Dynamics Society of Canada. [Toronto, Ont.?]: CFD Society of Canada, 1994.

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Conference of the CFD Society of Canada (3rd 1995 Banff, Alta.). CFD 95: Third annual Conference of the CFD Society of Canada proceedings = La troisième conference annuelle de la société canadienne de CFD : comptes rendues : Banff, Alberta, June 25-27, 1995. Edited by Thibault Paul A, Bergeron Denis M, and Computational Fluid Dynamics Society of Canada. [S.l.]: Computational Fluid Dynamics Society of Canada, 1995.

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J, Baker A., and United States. National Aeronautics and Space Administration., eds. An arbitrary grid CFD algorithm for configuration aerodynamics analysis. Knoxville, TN: Computational Mechanics Corp., 1993.

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A, Orzechowski J., Baker A. J, and United States. National Aeronautics and Space Administration., eds. An arbitrary grid CFD algorithm for configuration aerodynamics analysis. Knoxville, TN: Computational Mechanics Corp., 1992.

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Association for Iron & Steel Technology, Minerals, Metals and Materials Society. Extraction and Processing Division. Process Technology and Modeling Committee, TMS Solidification Committee, and Minerals, Metals and Materials Society. Annual Meeting, eds. CFD modeling and simulation in materials processing. Hoboken, N.J: John Wiley & Sons, 2012.

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D, Robertson David, Moyer Seth A, and Ames Research Center, eds. An integrated CFD/experimental analysis of aerodynamic forces and moments. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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Book chapters on the topic "CFD analysis"

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Hailu, Getu, Michal Varchola, and Peter Hlbocan. "CFD Analysis in Turbomachinery." In Design of Hydrodynamic Machines, 195–244. New York: CRC Press, 2022. http://dx.doi.org/10.1201/9781003007142-9.

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Kumar, Swapnil, K. Sai Kiran, and Thundil Karuppa Raj Rajagopal. "CFD Analysis of Automotive Radiators." In Advances in Automotive Technologies, 1–7. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-5947-1_1.

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Patel, Rishika, Shital Patel, and S. N. Teli. "CFD Analysis of Air-Swirl Burner." In Proceedings of International Conference on Intelligent Manufacturing and Automation, 561–67. Singapore: Springer Nature Singapore, 2023. http://dx.doi.org/10.1007/978-981-19-7971-2_54.

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Kumarasamy, G. S., V. P. M. Baskaralal, and S. Arunkumar. "Modeling and CFD Analysis of Gerotor Pump." In Proceedings of 2nd International Conference on Intelligent Computing and Applications, 327–39. Singapore: Springer Singapore, 2016. http://dx.doi.org/10.1007/978-981-10-1645-5_27.

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Wiedermann, Alexander. "CFD for Turbomachinery Blading Analysis and Design." In Advances in Fluid Mechanics and Turbomachinery, 29–38. Berlin, Heidelberg: Springer Berlin Heidelberg, 1998. http://dx.doi.org/10.1007/978-3-642-72157-1_3.

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Sharma, Atul. "Introduction to CFD: Development, Application, and Analysis." In Introduction to Computational Fluid Dynamics, 19–33. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-72884-7_2.

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Amin, Mihir H., Monil M. Bhamare, Ayush V. Patel, Darsh P. Pandya, Rutvik M. Bhavsar, and Snehal N. Patel. "CFD Analysis Applied to Hydrodynamic Journal Bearing." In Information and Communication Technology for Intelligent Systems, 755–76. Singapore: Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-7062-9_76.

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Ma, Guowei, Yimiao Huang, and Jingde Li. "VCE Overpressure Prediction by CFD Modelling." In Risk Analysis of Vapour Cloud Explosions for Oil and Gas Facilities, 45–79. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-7948-2_3.

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Wentsch, Marlene. "The 3D-CFD Tool QuickSim." In Analysis of Injection Processes in an Innovative 3D-CFD Tool for the Simulation of Internal Combustion Engines, 21–34. Wiesbaden: Springer Fachmedien Wiesbaden, 2018. http://dx.doi.org/10.1007/978-3-658-22167-6_3.

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Stoevesandt, Bernhard, Robert Stresing, Andrei Shishkin, Claus Wagner, and Joachim Peinke. "Multi-scale Analysis of Turbulence in CFD-Simulations." In Springer Proceedings in Physics, 41–44. Berlin, Heidelberg: Springer Berlin Heidelberg, 2012. http://dx.doi.org/10.1007/978-3-642-28968-2_9.

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Conference papers on the topic "CFD analysis"

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Ostman, A., and I. J. Oye. "Rans Solver Applied For Hydrodynamic Analysis of Twin-Hull Ferry." In CFD 2003: CFD Technology In Ship Hydrodynamics. RINA, 2003. http://dx.doi.org/10.3940/rina.cfd.2003.8.

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Southall, N., and B. Corlett. "Basin – Development of A Practical Boundary Element Code For Hydrodynamic Analysis." In CFD 2005- CFD Technology in Ship Hydrodynamics. RINA, 2005. http://dx.doi.org/10.3940/rina.cfd.2005.5.

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Pittalaga, C., and P. Becchi. "Comparison Between Ranse Calculations and Panel Method Results For The Hydrodynamic Analysis of Marine Propellers." In CFD 2005- CFD Technology in Ship Hydrodynamics. RINA, 2005. http://dx.doi.org/10.3940/rina.cfd.2005.9.

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Yesilel, H., F. O. Edis, Theodore E. Simos, George Psihoyios, and Ch Tsitouras. "Ship Airwake Analysis by CFD Methods." In Numerical Analysis and Applied Mathematics. AIP, 2007. http://dx.doi.org/10.1063/1.2790239.

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Bosschers, J., G. Vaz, A. R. Starke, and E. van Wijngaarden. "Computational Analysis of Propeller Sheet Cavitation and Propeller-Ship Interaction." In Marine CFD 2008. RINA, 2008. http://dx.doi.org/10.3940/rina.cfd.2008.03.

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Li, Lei, Carlos Lange, and Yongsheng Ma. "Intelligent CFD Analysis Regime Validation and Selection in Feature-based Cyclic CAD/CFD Interaction Process." In CAD'17. CAD Solutions LLC, 2017. http://dx.doi.org/10.14733/cadconfp.2017.263-267.

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Hosder, Serhat, Bernard Grossman, Raphael Haftka, William Mason, and Layne Watson. "Observations on CFD Simulation Uncertainties." In 9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-5531.

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Rampidis, I., A. Nikolopoulos, N. Koukouzas, P. Grammelis, E. Kakaras, Theodore E. Simos, George Psihoyios, and Ch Tsitouras. "Optimization of Computational Performance and Accuracy in 3-D Transient CFD Model for CFB Hydrodynamics Predictions." In Numerical Analysis and Applied Mathematics. AIP, 2007. http://dx.doi.org/10.1063/1.2790176.

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Bazarov, Vladimir, Jose Hinckel, and Helcio Villa Nova. "CFD Analysis of Swirl Atomizers." In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-5229.

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Na, Sangkwon, Bin Zhu, M. Bryden, and Tom Shih. "CFD Analysis of Film Cooling." In 44th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-22.

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Reports on the topic "CFD analysis"

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Lee, S. SDI CFD MODELING ANALYSIS. Office of Scientific and Technical Information (OSTI), May 2011. http://dx.doi.org/10.2172/1014152.

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Lee, S. TANK48 CFD MODELING ANALYSIS. Office of Scientific and Technical Information (OSTI), May 2011. http://dx.doi.org/10.2172/1016386.

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Tzanos, C. P. Status report : guard containment CFD analysis. Office of Scientific and Technical Information (OSTI), March 2006. http://dx.doi.org/10.2172/924681.

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Richard W. Johnson, Hiroyuki Sato, and Richard R. Schultz. CFD Analysis of Core Bypass Phenomena. Office of Scientific and Technical Information (OSTI), November 2009. http://dx.doi.org/10.2172/974775.

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Richard W. Johnson, Hiroyuki Sato, and Richard R. Schultz. CFD Analysis of Core Bypass Phenomena. Office of Scientific and Technical Information (OSTI), March 2010. http://dx.doi.org/10.2172/978363.

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Finlayson, Elizabeth U., Buvana Jayaraman, Astrid R. Kristoffersen, and Ashok J. Gadgil. CFD analysis of LLNL downdraft table. Office of Scientific and Technical Information (OSTI), October 2003. http://dx.doi.org/10.2172/817257.

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Choi, Bongkeun, Byungjae Ahn, Jeonggook Paek, and Dongsin Kim. CFD Analysis of Center-Mounted HVAC System. Warrendale, PA: SAE International, May 2005. http://dx.doi.org/10.4271/2005-08-0329.

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Wang, Weimin, Satoshi Sasaki, and Masaki Kakizawa. Thermal Analysis for a Radiator Using CFD. Warrendale, PA: SAE International, May 2005. http://dx.doi.org/10.4271/2005-08-0332.

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Sturek, Walter B., Taylor Sr., and Malcolm S. Statistical Analysis of CFD Results for Missile Surface Pressures. Fort Belvoir, VA: Defense Technical Information Center, September 2001. http://dx.doi.org/10.21236/ada394691.

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Hassan, Yassin A., and Victor M. Ugaz. Experimental and CFD Analysis of Advanced Convective Cooling Systems. Office of Scientific and Technical Information (OSTI), June 2012. http://dx.doi.org/10.2172/1050435.

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