Relevant bibliographies by topics / Computational fluid dynamic

Academic literature on the topic 'Computational fluid dynamic'

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Published: 4 June 2021
Last updated: 8 June 2024

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Journal articles on the topic "Computational fluid dynamic"

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Raza, Md Shamim, Nitesh Kumar, and Sourav Poddar. "Combustor Characteristics under Dynamic Condition during Fuel – Air Mixingusing Computational Fluid Dynamics." Journal of Advances in Mechanical Engineering and Science 1, no. 1 (August 8, 2015): 20–33. http://dx.doi.org/10.18831/james.in/2015011003.

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Gao, Feng, Gang Li, Rui Hu, and Hiroshi Okada. "Computational Fluid Dynamic Analysis of Coronary Artery Stenting." International Journal of Bioscience, Biochemistry and Bioinformatics 4, no. 3 (2014): 155–59. http://dx.doi.org/10.7763/ijbbb.2014.v4.330.

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Storti, Mario A., Norberto M. Nigro, Rodrigo R. Paz, and Lisandro D. Dalcín. "Dynamic boundary conditions in computational fluid dynamics." Computer Methods in Applied Mechanics and Engineering 197, no. 13-16 (February 2008): 1219–32. http://dx.doi.org/10.1016/j.cma.2007.10.014.

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Iaronka, Odirlan, Vitor Cristiano Bender, and Tiago Bandeira Marchesan. "Thermal Management Of Led Luminaires Based On Computational Fluid Dynamic." Eletrônica de Potência 20, no. 1 (February 1, 2015): 76–84. http://dx.doi.org/10.18618/rep.2015.1.076084.

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Ronch, A. Da, D. Vallespin, M. Ghoreyshi, and K. J. Badcock. "Evaluation of Dynamic Derivatives Using Computational Fluid Dynamics." AIAA Journal 50, no. 2 (February 2012): 470–84. http://dx.doi.org/10.2514/1.j051304.

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Tharehalli Mata, Gurubasavaraju, Hemantha Kumar, and Arun Mahalingam. "Performance analysis of a semi-active suspension system using coupled CFD-FEA based non-parametric modeling of low capacity shear mode monotube MR damper." Proceedings of the Institution of Mechanical Engineers, Part D: Journal of Automobile Engineering 233, no. 5 (April 10, 2018): 1214–31. http://dx.doi.org/10.1177/0954407018765899.

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In this work, an approach for formulation of a non-parametric-based polynomial representative model of magnetorheological damper through coupled computational fluid dynamics and finite element analysis is presented. Using this, the performance of a quarter car suspension subjected to random road excitation is estimated. Initially, prepared MR fluid is characterized to obtain a relationship between the field-dependent shear stress and magnetic flux density. The amount of magnetic flux induced in the shear gap of magnetorheological damper is computed using finite element analysis. The computed magnetic field is used in the computational fluid dynamic analysis to calculate the maximum force induced under specified frequency, displacement and applied current using ANSYS CFX software. Experiments have been conducted to verify the credibility of the results obtained from computational analysis, and a comparative study has been made. From the comparison, it was found that a good agreement exists between experimental and computed results. Furthermore, the influence of fluid flow gap length and frequency on the induced force of the damper is investigated using the computational methods (finite element analysis and computational fluid dynamic) for various values. This proposed approach would serve in the preliminary design for estimation of magnetorheological damper dynamic performance in semi-active suspensions computationally prior to experimental analysis.
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Taherian, Shahab, Hamid Rahai, Bernardo Gomez, Thomas Waddington, and Farhad Mazdisnian. "Computational fluid dynamics evaluation of excessive dynamic airway collapse." Clinical Biomechanics 50 (December 2017): 145–53. http://dx.doi.org/10.1016/j.clinbiomech.2017.10.018.

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Tao, Jin, Qinglin Sun, Wei Liang, Zengqiang Chen, Yingping He, and Matthias Dehmer. "Computational fluid dynamics based dynamic modeling of parafoil system." Applied Mathematical Modelling 54 (February 2018): 136–50. http://dx.doi.org/10.1016/j.apm.2017.09.008.

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Lu, Bao Yan, and Yan Zhou Li. "Computational Fluid Dynamic of Date Transfer." Applied Mechanics and Materials 477-478 (December 2013): 236–39. http://dx.doi.org/10.4028/www.scientific.net/amm.477-478.236.

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A high-speed craft in the supersonic speed, ambient temperature and pressure would affect its structure, heat flow fluid-solid coupling simulation can quantify the effect. Due to physical fields had different heat flow fluid-solid coupling simulation, the data transmission was needed when the fluid dynamics to calculate the quantities of the import structure field. This paper given the derivation process and method of the physical fields data transfer, fluid dynamics to calculate the data in the simulation of structure field was implemented and to quantify the temperature field and stress field impacted on structure field.
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Choi, Seongim, Anubhav Datta, and Juan J. Alonso. "Prediction of Helicopter Rotor Loads Using Time-Spectral Computational Fluid Dynamics and an Exact Fluid–Structure Interface." Journal of the American Helicopter Society 56, no. 4 (October 1, 2011): 1–15. http://dx.doi.org/10.4050/jahs.56.042001.

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The objectives of this paper are to introduce time-spectral computational fluid dynamics (CFD) for the analysis of helicopter rotor flows in level flight and to introduce an exact fluid–structure interface for coupled CFD/computational structural dynamics (CSD) analysis. The accuracy and efficiency of time-spectral CFD are compared with conventional time-marching computations. The exact interface is equipped with an exact delta coupling procedure that bypasses the requirement for sectional airloads. Predicted loads are compared between time-spectral and time-marching CFD using both interfaces and validated using UH-60A flight data for high-vibration and dynamic stall conditions. It is concluded that time-spectral CFD can indeed predict rotor performance and peak-to-peak structural loads efficiently, and hence, open opportunity for blade shape optimization. The vibratory and dynamic stall loads, however, require a large number of time instances, which reduces its efficiency. The exact interface and delta procedure allow coupling to be implemented for arbitrary grids and advanced structural models exactly, without the requirement for two-dimensional sectional airloads.
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Dissertations / Theses on the topic "Computational fluid dynamic"

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Da, Ronch Andrea. "On the calculation of dynamic derivatives using computational fluid dynamics." Thesis, University of Liverpool, 2012. http://livrepository.liverpool.ac.uk/5513/.

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In this thesis, the exploitation of computational fluid dynamics (CFD) methods for the flight dynamics of manoeuvring aircraft is investigated. It is demonstrated that CFD can now be used in a reasonably routine fashion to generate stability and control databases. Different strategies to create CFD-derived simulation models across the flight envelope are explored, ranging from combined low-fidelity/high-fidelity methods to reduced-order modelling. For the representation of the unsteady aerodynamic loads, a model based on aerodynamic derivatives is considered. Static contributions are obtained from steady-state CFD calculations in a routine manner. To more fully account for the aircraft motion, dynamic derivatives are used to update the steady-state predictions with additional contributions. These terms are extracted from small-amplitude oscillatory tests. The numerical simulation of the flow around a moving airframe for the prediction of dynamic derivatives is a computationally expensive task. Results presented are in good agreement with available experimental data for complex geometries. A generic fighter configuration and a transonic cruiser wind tunnel model are the test cases. In the presence of aerodynamic non-linearities, dynamic derivatives exhibit significant dependency on flow and motion parameters, which cannot be reconciled with the model formulation. An approach to evaluate the sensitivity of the non-linear flight simulation model to variations in dynamic derivatives is described. The use of reduced models, based on the manipulation of the full-order model to reduce the cost of calculations, is discussed for the fast prediction of dynamic derivatives. A linearized solution of the unsteady problem, with an attendant loss of generality, is inadequate for studies of flight dynamics because the aircraft may experience large excursions from the reference point. The harmonic balance technique, which approximates the flow solution in a Fourier series sense, retains a more general validity. The model truncation, resolving only a small subset of frequencies typically restricted to include one Fourier mode at the frequency at which dynamic derivatives are desired, provides accurate predictions over a range of two- and three-dimensional test cases. While retaining the high fidelity of the full-order model, the cost of calculations is a fraction of the cost for solving the original unsteady problem. An important consideration is the limitation of the conventional model based on aerodynamic derivatives when applied to conditions of practical interest (transonic speeds and high angles of attack). There is a definite need for models with more realism to be used in flight dynamics. To address this demand, various reduced models based on system-identification methods are investigated for a model case. A non-linear model based on aerodynamic derivatives, a multi-input discrete-time Volterra model, a surrogate-based recurrence-framework model, linear indicial functions and radial basis functions trained with neural networks are evaluated. For the flow conditions considered, predictions based on the conventional model are the least accurate. While requiring similar computational resources, improved predictions are achieved using the alternative models investigated. Furthermore, an approach for the automatic generation of aerodynamic tables using CFD is described. To efficiently reduce the number of high-fidelity (physics-based) analyses required, a kriging-based surrogate model is used. The framework is applied to a variety of test cases, and it is illustrated that the approach proposed can handle changes in aircraft geometry. The aerodynamic tables can also be used in real-time to fly the aircraft through the database. This is representative of the role played by CFD simulations and the potential impact that high-fidelity analyses might have to reduce overall costs and design cycle time.
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Hickerson, David A. "Computational Fluid Dynamic Study of Heaving-to." Thesis, Virginia Tech, 2013. http://hdl.handle.net/10919/23766.

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This study looks at the fluid interactions from the wake of a sail boat performing the heaving-to storm tactic in heavy weather seas with the waves. This interaction causes the wave height in the wake to be reduced. The fluid flow in the top layer of the wave is seen to move with the wake as the hull drifts with the wind. This movement of the top layer of the wave provides a vertical momentum cancelation affect with the portion of the wave that it moves over reducing the wave height. STAR-CCM+ CFD software is used to perform the simulations of the steep waves with wavelength of 25 meters, 55 meters, and 67 meters. In the simulation, a propulsive force is used to simulate the wind force on the boat.
Master of Science
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Molale, Dimpho Millicent. "A computational evaluation of flow through porous media." Thesis, Link to the online version, 2007. http://hdl.handle.net/10019/686.

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Chambers, Steven B. "Investigation of combustive flows and dynamic meshing in computational fluid dynamics." Thesis, Texas A&M University, 2004. http://hdl.handle.net/1969.1/1324.

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Computational Fluid Dynamics (CFD) is a field that is constantly advancing. Its advances in terms of capabilities are a result of new theories, faster computers, and new numerical methods. In this thesis, advances in the computational fluid dynamic modeling of moving bodies and combustive flows are investigated. Thus, the basic theory behind CFD is being extended to solve a new class of problems that are generally more complex. The first chapter that investigates some of the results, chapter IV, discusses a technique developed to model unsteady aerodynamics with moving boundaries such as flapping winged flight. This will include mesh deformation and fluid dynamics theory needed to solve such a complex system. Chapter V will examine the numerical modeling of a combustive flow. A three dimensional single vane burner combustion chamber is numerically modeled. Species balance equations along with rates of reactions are introduced when modeling combustive flows and these expressions are discussed. A reaction mechanism is validated for use with in situ reheat simulations. Chapter VI compares numerical results with a laminar methane flame experiment to further investigate the capabilities of CFD to simulate a combustive flow. A new method of examining a combustive flow is introduced by looking at the solutions ability to satisfy the second law of thermodynamics. All laminar flame simulations are found to be in violation of the entropy inequality.
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Clinkinbeard, Nicholus Ryan. "Computational fluid dynamic modeling of acoustic liquid manipulation." [Ames, Iowa : Iowa State University], 2006.

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CARDILLO, GIULIA. "Fluid Dynamic Modeling of Biological Fluids: From the Cerebrospinal Fluid to Blood Thrombosis." Doctoral thesis, Politecnico di Torino, 2020. http://hdl.handle.net/11583/2845786.

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Mora, Acosta Josue. "Numerical algorithms for three dimensional computational fluid dynamic problems." Doctoral thesis, Universitat Politècnica de Catalunya, 2001. http://hdl.handle.net/10803/6685.

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The target of this work is to contribute to the enhancement of numerical methods for the simulation of complex thermal systems. Frequently, the factor that limits the accuracy of the simulations is the computing power: accurate simulations of complex devices require fine three-dimensional discretizations and the solution of large linear equation systems.
Their efficient solution is one of the central aspects of this work. Low-cost parallel computers, for instance, PC clusters, are used to do so. The main bottle-neck of these computers is the notwork, that is too slow compared with their floating-point performance.
Before considering linear solution algorithms, an overview of the mathematical models used and discretization techniques in staggered cartesian and cylindrical meshes is provided.
The governing Navier-Stokes equations are solved using an implicit finite control volume method. Pressure-velocity coupling is solved with segregated approaches such as SIMPLEC.
Different algorithms for the solution of the linear equation systems are reviewed: from incomplete factorizations such as MSIP, Krylov solvers such as BICGSTAB and GMRESR to acceleration techniques such as the Algebraic Multi Grid and the Multi Resolution Analysis with wavelts. Special attention is paid to preconditioned Krylov solvers for their application to parallel CFD problems.
The fundamentals of parallel computing in distributed memory computers as well as implemetation details of these algorithms in combination with the domain decomposition method are given. Two different distributed memory computers, a Cray T3E and a PC cluster are used for several performance measures, including network throughput, performance of algebraic subroutines that affect to the overall efficiency of algorithms, and the solver performance. These measures are addressed to show the capabilities and drawbacks of parallel solvers for several processors and their partitioning configurations for a problem model.
Finally, in order to illustrate the potential of the different techniques presented, a three-dimensional CFD problem is solved using a PC cluster. The numerical results obtained are validated by comparison with other authors. The speedup up to 12 processors is measured. An analysis of the computing time shows that, as expected, most of the computational effort is due to the pressure-correction equation,here solved with BiCGSTAB. The computing time algorithm , for different problem sizes, is compared with Schur-Complement and Multigrid.
El trabajo de tesis se centra en la solución numérica de las ecuaciones de navier-Stokes en regimen transitorio, tridimensional y laminar. Los algoritmos utilizados son del tipo segregado (SIMPLEC)y se basan en el uso de técnicas de volumenes finitos, con mallas estructurales del tipo staggered y discretizaciones temporales implícitas. En este contexto, el pricipal, problema son los elevados tiempos de cálculo de las simulaciones, que en buena parte se deben a la solución de los sistemas de ecuaciones lineales. Se hace una revisión de diferentes métodos utilizados típicamente en ordenadores secuenciales: GMRES, BICGSTAB, ACM, MSPIP.
A fin de reducir los tiempos de cálculo se emplean ordenadores paralelos de memoria distribuida, basados en la agrupacion de ordenadores personales convencionales (PC clusters). Por lo que respecta a la potencia de cálculo por procesador, estos sistemas son comparables a los ordenadores paralelos de memoria distribuida convencionales (como el Cray T3E) siendo, su principal problema la baja capacidad de comunicación (elevada latencia, bajo ancho de banda). Este punto condiciona toda la estrategia computacional, obligando a reducir al máximo el número y el tamaño de los mensajes intercambiados. Este aspecto se cuantifica detalladamente en la tesis, realizando medidas de tiempos de cálculo en ambos ordenadores para diversas operaciones críticas para los algoritmos lineales. Tambien se miden y comparan los tiempos de cálculo y speed ups obtenidos en la solución de los sistemas lineales con diferentes algoritmos paralelos (Jacobi, MSIP, GMRES, BICGSTAB) y para diferentes tamaños de malla.
Finalmente, se utilizan las técnicas anteriores para resolver el caso denominado driven cavity, en situacionies tridimensionales y con numeros de Reynolds de hasta 8000. Los resultados obtenidos se utilizan para validar los códigos desarrollados, en base a resultados de otros códigos y también se basa en la comparación con resultados experimentales procedentes de la bibliografía. Se utilizan hasta 12 procesadores, obteniendose spped ups de hasta 9.7 en el cluster de PCs. Se analizan los tiempos de cálculo de cada fase del código, señalandose areas para futuras mejoras. Se comparan los tiempos de cálculo con los algoritmos implementados en otros trabajos. La conclusión final es que los clusters de PCs son una plataforma de gran potencia en los cálculos de dinámica de fluidos computacional.
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Coppel, Anna Louise. "A computational fluid dynamic investigation of rowing oar blades." Thesis, University of Birmingham, 2010. http://etheses.bham.ac.uk//id/eprint/793/.

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This thesis describes the application of computational fluid dynamics (CFD) to model the flow regime around rowing oar blades. The two phase flow that was present at the surface between the water and the air was also incorporated into the CFD model. Firstly, a quasi–static method was applied, whereby the blade was held at a discrete number of angles of attack to the oncoming flow. The performance of the model was assessed by applying it to four scaled oar blade designs and validating results against an experimental data set. The results were encouraging with lift and drag coefficients acting on the blades being well predicted throughout. The scope was extended to include full size oar blades of designs typically found in competition rowing. A second approach to investigating the flow around oar blades was also adopted, where instead of being held stationary, the blades moved in the fluid domain. The unsteady effects induced by this rotational motion were found to be substantial, with a 72% and 67% increase in the lift and drag coefficients respectively. Finally, through coupling the CFD predictions of oar blade force coefficients with a mathematical model of rowing, it was possible to determine the influence of oar blade design on rowing performance, and also use the mathematical model to further validate the CFD predictions against on–water data. The results provided an accurate assessment of boat performance during the rowing stroke.
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Irshad, Wahid. "Wind resource assessment : statistical and computational fluid-dynamic analysis." Thesis, Edinburgh Napier University, 2012. http://researchrepository.napier.ac.uk/Output/5329.

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Wind is an important source of renewable energy and is widely available, despite the changing condition. In recent years a growing number of manufacturers have produced small wind turbines suitable for utilisation by individual householders or small businesses. These systems are designed to install in towns or cities. This raises the question about the potential of wind energy resource in build-up areas. This thesis sets to investigate the wind energy resource implication in the build-up areas by understanding the wind climatology of urban areas. As well as the overall mean wind speed, knowledge of the wind speed distribution (due to the non-linear relationship between wind speed and wind power) and the wind-direction distribution for optimum turbine siting is required. Other areas that have been considered are short-duration fluctuations in both speed and direction as these can affect the efficiency of the turbine. The aims of this research are to study the local wind conditions and estimate the available wind resource for the wind-energy driven generation of electricity in Edinburgh by taking into account of its climate, wind data and topographical effects. To achieve these aims eleven years of Met office data was investigated in addition to analysis of the data collected from locally installed weather station. Diurnal effect on wind condition was studied and found to be more pronounced in Edinburgh's rural area than its urban conurbation. It was also found that the available wind energy in the urban area is 30% less than that of the rural area. Turbulence in wind speed and direction of flow was also investigated. Careful consideration of all the parameters defining and affecting the prevailing wind revealed the wind resource in Edinburgh's urban area to be insufficient for viable generation of wind energy through the available technology of micro WEC (wind energy converter) systems. A CFD analysis was also performed to determine wind resource differences because of different mounting locations of wind equipment over the building under consideration. As a part of the project, a commercially available wind turbine was installed and monitored to investigate its performance in urban area. The research study finally suggests that the available grid connected micro WEC system cannot provide a cost effective contribution to urban Edinburgh's renewable energy generation.
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Gao, Rui. "Computational Fluid Dynamic and Rotordynamic Study on the Labyrinth Seal." Diss., Virginia Tech, 2012. http://hdl.handle.net/10919/28134.

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The labyrinth seal is widely used in turbo machines to reduce leakage flow. The stability of the rotor is influenced by the labyrinth seal because of the driving forces generated in the seal. The working fluid usually has a circumferential velocity component before entering the seal; the ratio of circumferential velocity and shaft synchronous surface velocity is defined as pre-swirl rate. It has been observed that pre-swirl rate is an important factor affecting driving forces in the labyrinth seal thus affecting the stability of the rotor. Besides the pre-swirl, the eccentricity, the clearance, and the configuration of tooth locations are all factors affecting the rotordynamic properties of the labyrinth seal. So it is of interest to investigate the exact relationships between those factors and the sealâ s rotordynamic properties. In this research, three types of labyrinth seals have been modeled: the straight eye seal, the stepped eye seal, and the balance drum seal. For the straight eye seal, a series of models were built to study the influence of eccentricity and clearance. The other two seals each have only one model. All models were built with Solid Works and meshed with ANSYS-ICEM. Flows in those models were simulated by numerically solving the Reynolds-Averaged Navier-Stokes (RANS) equations in the ANSYS-CFX and then rotordynamic coefficients for each seal were calculated based on the numerical results. It had previously been very difficult to generate a pre-swirl rate higher than 60% in a numerical simulation. So three ways to create pre-swirl in ANSYS-CFX were studied and finally the method by specifying the inlet velocity ratio was employed. Numerical methods used in this research were introduced including the frame transfer, the k-ε turbulence model with curvature correction, and the scalable wall function. To obtain the optimal mesh and minimize the discretization error, a systematical grid study was conducted including grid independence studies and discretization error estimations. Some of the results were compared with previous bulk-flow or experimental results to validate the numerical model and method. The fluid field in the labyrinth seal must be analyzed before conducting rotordynamic analysis. The predicted pressure distributions and leakages were compared with bulk-flow results. A second small vortex at the downstream edge of each tooth was found in the straight eye seal. This has never been reported before and the discovery of this small vortex will help to improve seal designs in the future. The detailed flows in discharged region and in chambers were also discussed. Radial and tangential forces on the rotor were solved based on the fluid field results. It is shown that the traditional first-order rotordynamic model works well for low pre-swirl cases but does not accurately reflect the characteristics for high pre-swirl cases. For example compressor eye seals usually have pre-swirl rates bigger than 70% and the second order model is required. Thus a second-order model including inertia terms was built and applied to the rotordynamic analysis in this research. The influence of pre-swirl, eccentricity and clearance were studied using the straight eye seal model. The rotordynamic characteristics of the stepped eye seal and the balance drum seal were studied considering high pre-swirl rates. Some relationships between influencing factors and the four rotordynamic coefficients were concluded. The results also showed that for all the three seals higher pre-swirl leads to higher cross-coupled stiffness which is one of the main factors causing rotor instability. The rotor stability analysis was conducted to study the influence of drum balance seal on the stability. The rotor was designed with typical dimensions and natural frequencies for a centrifugal compressor rotor. The parameters for bearing and aerodynamic force were also set according to general case in compressors to minimize the effects from them. The result shows that the high pre-swirl rate in balance drum seal leads to rotor instability, which confirmed the significant effect of pre-swirl on the seal and the rotor system.
Ph. D.
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Books on the topic "Computational fluid dynamic"

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AIAA Computational Fluid Dynamics Conference (11th 1993 Orlando, Fla.). 11th AIAA Computational Fluid Dynamics Conference: July 6-9, 1993, Orlando, Florida. New York: AIAA, 1993.

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AIAA Computational Fluid Dynamics Conference (14th 1999 Norfolk, Virginia). A collection of technical papers: 14th AIAA Computational Fluid Dynamics Conference, Norfolk, Virginia, 28 June-1 July 1999. Reston, Va: American Institute of Aeronautics and Astronautics, 1999.

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AIAA Computational Fluid Dynamics Conference (13th 1997 Snowmass Village, Co.). A collection of technical papers: 13th AIAA Computational Fluid Dynamics Conference ; Snowmass Village, CO, June 29-July 2, 1997. Reston, Va: American Institute of Aeronautics and Astronautics, 1997.

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Wilcox, David C. Turbulence modeling for CFD. La Cãnada, CA: DCW Industries, Inc., 1993.

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Wilcox, David C. Turbulence modeling for CFD. 2nd ed. La Cãnada, Calif: DCW Industries, 1998.

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Wilcox, David C. Turbulence modeling for CFD. La Cañada, CA: DCW Industries, 1994.

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Meng-Sing, Liou, Hindman Richard G, and United States. National Aeronautics and Space Administration., eds. An approach for dynamic grids. [Washington, DC]: National Aeronautics and Space Administration, 1994.

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American Institute of Aeronautics and Astronautics, ed. 12th AIAA Computational Fluid Dynamics Conference: A collection of technical papers ; June 19-22, 1995/San Diego, CA. Washington, D.C.]: American Institute of Aeronautics and Astronautics, 1995.

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A, Ladd J., Yuhas A. J, and United States. National Aeronautics and Space Administration., eds. Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach. [Washington, DC: National Aeronautics and Space Administration, 1996.

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Kuhn, Gary D. Postflight aerothermodynamic analysis of Pegasus[copyright] using computational fluid dynamic techniques. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.

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Book chapters on the topic "Computational fluid dynamic"

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Anderson, J. D. "Mathematical Properties of the Fluid Dynamic Equations." In Computational Fluid Dynamics, 77–86. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-85056-4_4.

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Anderson, J. D. "Mathematical Properties of the Fluid Dynamic Equations." In Computational Fluid Dynamics, 75–84. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-662-11350-9_4.

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Elizarova, Tatjana G. "Quasi-gas-dynamic Equations." In Computational Fluid and Solid Mechanics, 37–62. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-00292-2_3.

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Schmidt, Gunar, Hendrik C. Kuhlmann, and Hans J. Rath. "Instabilities of Dynamic Thermo- and Solutocapillary Liquid Layers." In Computational Fluid Dynamics 2000, 285–90. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-642-56535-9_41.

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Fauconnier, Dieter, Chris De Langhe, and Erik Dick. "The Sampling Based Dynamic Procedure for Numerical Discretization Enhancement." In Computational Fluid Dynamics 2006, 481–86. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-540-92779-2_75.

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Dadone, Andrea, and Bernard Grossman. "Design Optimization of Fluid Dynamic Problems Using Cartesian Grids." In Computational Fluid Dynamics 2002, 591–96. Berlin, Heidelberg: Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-642-59334-5_89.

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Pogorelov, Nikolai V. "Numerical Modeling of Discontinuous Gas Dynamic and MHD Astrophysical Flows." In Computational Fluid Dynamics 2000, 145–50. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-642-56535-9_19.

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Bogey, Christophe, Nicolas de Cacqueray, and Christophe Bailly. "A Dynamic Spatial Filtering Procedure for Shock Capturing in High-Order Computations." In Computational Fluid Dynamics 2008, 417–22. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-01273-0_53.

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Naitoh, Ken. "Cytofluid Dynamic Theory for Calculating Two-phase Flows and Bio-chemical Reactions." In Computational Fluid Dynamics 2000, 781–82. Berlin, Heidelberg: Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-642-56535-9_127.

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Jaouad, H., P. Vikram, E. Balasubramanian, and G. Surendar. "Computational Fluid Dynamic Analysis of Amphibious Vehicle." In Lecture Notes on Multidisciplinary Industrial Engineering, 303–13. Singapore: Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-8468-4_23.

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Conference papers on the topic "Computational fluid dynamic"

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Hartley, Tom T., and Alex DeAbreu-Garcia. "Computational Fluid Dynamic Control." In 1989 American Control Conference. IEEE, 1989. http://dx.doi.org/10.23919/acc.1989.4790276.

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Pierart, Fabian G., Daniel A. Vergara Sanhueza, and Santiago Riquelme. "Greenhouse Parametric Computational Fluid Dynamic model." In 2022 IEEE International Conference on Automation/XXV Congress of the Chilean Association of Automatic Control (ICA-ACCA). IEEE, 2022. http://dx.doi.org/10.1109/ica-acca56767.2022.10005984.

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Karmakar, Subrata, and R. Lal Kushwaha. "Dynamic Analysis of Soil Tillage Using Computational Fluid Dynamics." In 2005 SAE Commercial Vehicle Engineering Conference. 400 Commonwealth Drive, Warrendale, PA, United States: SAE International, 2005. http://dx.doi.org/10.4271/2005-01-3571.

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VENKATESWARAN, SANKARAN, JEFFREY GRENDA, and CHARLES MERKLE. "Computational fluid dynamic analysis of liquid rocket combustion instability." In 10th Computational Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-1609.

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Potturi, Amarnatha Sarma, and Oshin Peroomian. "Dynamic Stability Analysis of the Orion Crew Module through Computational Fluid Dynamics." In 46th AIAA Fluid Dynamics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-3200.

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Baker, Timothy, and Peter Cavallo. "Dynamic adaptation for deforming tetrahedral meshes." In 14th Computational Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-3253.

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Parthasarathy, Girija, and Dinkar Mylaraswamy. "Computational Fluid Dynamic Modeling for Engine Diagnosis." In ASME Turbo Expo 2003, collocated with the 2003 International Joint Power Generation Conference. ASMEDC, 2003. http://dx.doi.org/10.1115/gt2003-38567.

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This paper presents the results of a demonstration problem where computational fluid dynamics modeling (CFD) is used for engine diagnosis. As computational resources become faster and cheaper and detailed numerical models of heat transfer, fluid dynamics and chemical kinetics become more accurate, these numerical models can become viable alternatives for seeded fault tests. The work done here is one of the ways this could be done; that is, by using the results of a CFD model to map the effects of certain faults to a model parameter computed by a less detailed lumped parameter model.
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Rozario, Dexter, and Zoubir Zouaoui. "Computational Fluid Dynamic Analysis of Scramjet Inlet." In 45th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-30.

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Gnoffo, Peter. "Computational Fluid Dynamic Technology for Hypersonic Applications." In AIAA International Air and Space Symposium and Exposition: The Next 100 Years. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2003. http://dx.doi.org/10.2514/6.2003-2829.

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Dadone, A., B. Grossman, A. Dadone, and B. Grossman. "Progressive optimization of fluid dynamic design problems." In 13th Computational Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1997. http://dx.doi.org/10.2514/6.1997-1848.

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Reports on the topic "Computational fluid dynamic"

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Homicz, Gregory Francis. Computational Fluid Dynamic simulations of pipe elbow flow. Office of Scientific and Technical Information (OSTI), August 2004. http://dx.doi.org/10.2172/919140.

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Rokkam, Ram. Computational fluid dynamic modeling of fluidized-bed polymerization reactors. Office of Scientific and Technical Information (OSTI), January 2012. http://dx.doi.org/10.2172/1082969.

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Wurtzler, Kenneth, Amid Ansari, and Don Kinsey. Computational Fluid Dynamic Analysis of a Single-Engine Business Jet. Fort Belvoir, VA: Defense Technical Information Center, December 1996. http://dx.doi.org/10.21236/ada332966.

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Richard W. Johnson and Richard R. Schultz. Computational Fluid Dynamic Analysis of the VHTR Lower Plenum Standard Problem. Office of Scientific and Technical Information (OSTI), July 2009. http://dx.doi.org/10.2172/963762.

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Johnson, R. W., W. David Pointer, and Richard R. Schultz. Computational Fluid Dynamic Analysis for the Proposed VHTR Lower Plenum Standard Problem. Office of Scientific and Technical Information (OSTI), September 2008. http://dx.doi.org/10.2172/1389179.

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Sahu, Jubaraj, Gene R. Cooper, and Richard J. Benney. 3-D Parachute Descent Analysis Using Coupled Computational Fluid Dynamic and Structural Codes. Fort Belvoir, VA: Defense Technical Information Center, September 1997. http://dx.doi.org/10.21236/ada330375.

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Kokes, Joseph, Mark Costello, and Jubaraj Sahu. Generating an Aerodynamic Model for Projectile Flight Simulation Using Unsteady, Time Accurate Computational Fluid Dynamic Results. Fort Belvoir, VA: Defense Technical Information Center, September 2006. http://dx.doi.org/10.21236/ada457421.

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Hisley, Dixie, and Duane Frist. Performance of a Sequential and Parallel Computational Fluid Dynamic (CFD) Solver on a Missile Body Configuration. Fort Belvoir, VA: Defense Technical Information Center, August 1999. http://dx.doi.org/10.21236/ada368182.

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Norman, Logan, and Ram Srinivasan. Computational fluid dynamic modeling to determine the indoor environment of an electron-ion collider service building. Office of Scientific and Technical Information (OSTI), April 2022. http://dx.doi.org/10.2172/1964077.

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Groeneveld. L51673 The Development of a Ductile Pipe Fracture Model. Chantilly, Virginia: Pipeline Research Council International, Inc. (PRCI), May 1987. http://dx.doi.org/10.55274/r0010550.

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Covers a project to develop a fluid/structure/fracture interactive, inelastic-dynamic computational model for ductile fracture in gas transmission pipelines developed in cooperation with SNAM in Italy to infer specimen-size independent measures of the propagating fracture toughness from small-scale tests on line pipe materials. Verification by CSM on 56-in. diameter.See PR-15-527 (also L51673)
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