Academic literature on the topic 'Equations de Navier-Strokes'

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Journal articles on the topic "Equations de Navier-Strokes"

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Rogers, Stuart E., and Dochan Kwak. "An upwind differencing scheme for the incompressible navier–strokes equations." Applied Numerical Mathematics 8, no. 1 (1991): 43–64. http://dx.doi.org/10.1016/0168-9274(91)90097-j.

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Javed, A., K. Djijdeli, and J. T. Xing. "Shape adaptive RBF-FD implicit scheme for incompressible viscous Navier–Strokes equations." Computers & Fluids 89 (January 2014): 38–52. http://dx.doi.org/10.1016/j.compfluid.2013.10.028.

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Eggers, Jens, and Todd F. Dupont. "Drop formation in a one-dimensional approximation of the Navier–Stokes equation." Journal of Fluid Mechanics 262 (October 3, 1994): 205–21. http://dx.doi.org/10.1017/s0022112094000480.

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We consider the viscous motion of a thin axisymmetric column of fluid with a free surface. A one-dimensional equation of motion for the velocity and the radius is derived from the Navier–Strokes equation. We compare our results with recent experiments on the breakup of a liquid jet and on the bifurcation of a drop suspended from an orifice. The equations form singularities as the fluid neck is pinching off. The nature of the singularities is investigated in detail.
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Mao, Y., M. Buffat, and D. Jeandel. "Simulation of the Turbulent Flow Inside the Combustion Chamber of a Reciprocating Engine With a Finite Element Method." Journal of Fluids Engineering 116, no. 2 (1994): 363–69. http://dx.doi.org/10.1115/1.2910282.

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This paper presents numerical simulations of turbulent flows during the intake and the compression strokes of a model engine. The Favre average Navier-Stokes equations are solved with a k-ε turbulence model. The numerical procedure uses a time dependent semi-implicit scheme and a finite element method with a moving mesh (Buffat, 1991, Mao, 1990). Results of 2-D axisymmetrical calculations with and without inlet swirl are presented and compared to experimental data (Lance et al., 1991). The influence of different turbulence models and the numerical precision of the simulations are also discusse
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Meng, Fan Ming, Tao Yang, and Tao Long. "Study on Tribological Performances for Textured Bearing of ICE." Advanced Materials Research 690-693 (May 2013): 1999–2002. http://dx.doi.org/10.4028/www.scientific.net/amr.690-693.1999.

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The influence of dimples on the inner surface of big end bearing in internal combustion engine (ICE) on tribological performances of the bearing was investigated based on Navier-Strokes equation and other associated equations. In doing so, the CFD modulus in the software ANSYS12 version is used to analyze the dimple effect on the tribological performances of the bearing using two-way fluid-solid coupling algorithm. Some mechanisms are revealed about the dimple effect on the load-carrying capacity and friction coefficient of oil film, and the deformation and stress for the textured big end bear
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Shum, K. T. "A numerical study of the wave-induced solute transport above a rippled bed." Journal of Fluid Mechanics 299 (September 25, 1995): 267–88. http://dx.doi.org/10.1017/s0022112095003508.

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The role of wave-induced separated flow in solute transport above a rippled bed is studied from numerical solutions to the two-dimensional Navier–Strokes equations and the advection-diffusion equation. A horizontal ambient flow that varies sinusoidally in time is imposed far above the bed, and a constant concentration difference between the upper and lower boundaries of computation is assumed. The computed flow field is the sum of an oscillatory rectilinear flow and a vortical flow which is periodic both in time and in the horizontal. Poincaré sections of this flow suggest chaotic mixing. Vert
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E. Kirillov, Oleg, Ruslan M. Mirgazov, Yuri M. Ignatkin, Sergey G. Konstantinov, Pavel V. Makeev, and Mikhail Yu. Buntov. "Development of the Wind Tunnel CFD Model for Clarifying Rotor Blade Airfoil Unsteady Aerodynamic Researches." TEM Journal, May 27, 2021, 554–62. http://dx.doi.org/10.18421/tem102-10.

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A computational model of a wind tunnel (WT) with a special experimental rig has been developed directly for studying unsteady aerodynamic characteristics of a wing section with a helicopter blade profile. The model was constructed using CFD (Computational Fluid Dynamics) methods based on the URANS approach (Unsteady Reynolds Averaged Navier Strokes Equations). Therefore, the aerodynamic characteristics of the airfoil can be determined, taking into account influence of the WT walls such as walls perforation and various configurations of the experimental rig. Simulation of the flow around the wi
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Dissertations / Theses on the topic "Equations de Navier-Strokes"

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Bible, Stewart Andrew. "Study of the 'Poor Man's Navier Strokes' equation turbulence model." Lexington, Ky. : [University of Kentucky Libraries], 2003. http://lib.uky.edu/ETD/ukymeen2003t00104/Thesis.pdf.

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Thesis--University of Kentucky (M.S.), 2003.<br>Title from document title page. Document formatted into pages; contains ix, 110 p. : ill. Includes abstract and vita. Includes bibliographical references (p. 99-109).
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Rochoux, Mélanie Catherine. "Vers une meilleure prévision de la propagation d'incendies de forêt : évaluation de modèles et assimilation de données." Thesis, Châtenay-Malabry, Ecole centrale de Paris, 2014. http://www.theses.fr/2014ECAP0009/document.

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La prévision des incendies de forêt reste un défi puisque vitesse et direction de propagation dépendent des interactions multi-échelles entre la végétation, la topographie du terrain et les conditions météorologiques. Un modèle à l’échelle régionale peut donc difficilement prendre en compte le détail des processus physiques mis en jeu. Toute modélisation est entachée de nombreuses incertitudes (modélisation incomplète, méconnaissance du terrain, de la végétation et des interactions flamme/atmosphère, etc.) qu’il est nécessaire de quantifier et de corriger. Ces travaux de thèse proposent ainsi
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Jacq, Pascal. "Méthodes numériques de type Volumes Finis sur maillages non structurés pour la résolution de thermique anisotrope et des équations de Navier-Strokes compressibles." Thesis, Bordeaux, 2014. http://www.theses.fr/2014BORD0009/document.

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Lors de la rentrée atmosphérique nous sommes amenés à modéliser trois phénomènes physiques différents. Tout d'abord, l'écoulement autour du véhicule entrant dans l'atmosphère est hypersonique,il est caractérisé par la présence d'un choc fort et provoque un fort échauffement du véhicule. Nous modélisons l'écoulement par les équations de Navier-Stokes compressibles et l'échauffement du véhicule au moyen de la thermique anisotrope. De plus le véhicule est protégé par un bouclier thermique siège de réactions chimiques que l'on nomme communément ablation.Dans le premier chapitre de cette thèse nous
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Lubrano, Jean-Louis. "Etude théorique de la turbulence homogène soumise à des effets de rotation et modélisation en vue de l'implantation au sein d'un code résolvant les équations de Navier-Strokes." Ecully, Ecole centrale de Lyon, 1993. http://bibli.ec-lyon.fr/exl-doc/TH_T1482_jllubrano.pdf.

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La rotation a une influence certaine sur la turbulence homogène par le biais des forces de Coriolis. Ces effets, mal pris en compte par les modélisations classiques, nécessitent une approche plus élaborée. Un recours possible est la recherche d'informations dans l'espace spectral où les différents termes de l'équation du tenseur spectral ont une signification physique plus facile à appréhender. Ainsi a-t'il été mis clairement en évidence une partition de l'anisotropie en une composante caractérisant la directivité du champ énergétique et une composante définissant sa polarisation. Cette sépara
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Books on the topic "Equations de Navier-Strokes"

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A reduced order model of the linearized incompressible Navier-Strokes equations for the sensor/actuator placement problem. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 2000.

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Conference papers on the topic "Equations de Navier-Strokes"

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Morinishi, Koji, and Tomohiro Fukui. "Fluid-Structure Interactive Simulation Using a Virtual Flux Method." In ASME-JSME-KSME 2011 Joint Fluids Engineering Conference. ASMEDC, 2011. http://dx.doi.org/10.1115/ajk2011-20011.

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This paper describes the resent development of a virtual flux method for simulating fluid-structure interaction problems. The virtual flux method is one of the sharp interface Cartesian grid methods. The numerical flux across the interface is replaced with the virtual flux so that proper interface conditions must be satisfied there. In this study, the virtual flux method is applied to numerical flow simulations about reciprocating engines. The compressible Navier-Stokes equations are coupled with the equation of motion of the piston, connecting rod, and crank system. Intake and exhaust valves
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Verma, Ishan, Rakesh Yadav, Patrick Sharkey, Shaoping Li, and Ellen Meeks. "Modeling of Turbulent Swirl Stabilized Flame With Flamelet Generated Manifold and Hybrid LES-RANS Turbulence Model." In ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gt2019-91147.

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Abstract Hybrid turbulence modeling is a practical approach to efficiently model the wall-bounded turbulent flows. In this paper, a stress-blended eddy simulation (SBES) model is used with the flamelet generated manifold model (FGM) for modeling turbulent combustion. In the current SBES, the near-wall region is modeled using a two-equation k-ω Reynolds-averaged Navier-Strokes (RANS) formulation, and switches to a large eddy simulation (LES) model in the core region using a blending function. Similarly, the turbulence-related combustion modeling parameters, such as the variances in scalar trans
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Sharma, Himanshu, Murali Damodaran, and Pravinray Gandhi. "Computational Modeling of the Condensed Phase Aerosol Based Fire Extinguisher." In ASME 2014 4th Joint US-European Fluids Engineering Division Summer Meeting collocated with the ASME 2014 12th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/fedsm2014-21104.

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The computational modeling of a novel condensed phase aerosol based fire extinguisher is considered in this study to assess its operational details and performance. A solid propellant is present inside the canister which is ignited using piezoelectric actuators producing hot fire extinguishing gases. The cooling of these hot gases is facilitated by a matrix of chemically active cooling pellets placed along the canister which condenses hot gas and discharges solid aerosol particulates. The initial experimental investigation of the extinguisher carried out at the premises of an industrial partne
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Chen, Qingguang, Zhong Xu, Yulin Wu, and Yongjian Zhang. "Three-Dimensional Simulation of Turbulent Rectangular and Square Impinging Jet Flows." In ASME 2004 Heat Transfer/Fluids Engineering Summer Conference. ASMEDC, 2004. http://dx.doi.org/10.1115/ht-fed2004-56131.

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Flow characteristics of turbulent impinging jets issuing, respectively, from a rectangular and a square nozzles have been investigated numerically through the solution of three-dimensional Navier-Strokes equations in steady state. Two geometries with two nozzle-to-plate spacings of four and eight times of hydraulic diameters of the jet pipes, and two Reynolds numbers of 20000 and 30000 have been considered with fully developed inlet boundary conditions. An RNG based k–ε turbulence model and a deferred correction QUICK scheme in conjunction with the wall function method have been applied to the
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Ashok, Kumar S., Subramanian V. Anantha, and R. Vijayakumar. "Numerical Study on the Performance Analysis and Vibration Characteristics of Flexible Marine Propeller." In ASME 2020 39th International Conference on Ocean, Offshore and Arctic Engineering. American Society of Mechanical Engineers, 2020. http://dx.doi.org/10.1115/omae2020-18538.

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Abstract This paper addresses the hydro-elastic performance of two composite marine propellers at operating condition and compares the results with conventional materials. The study involves three stages namely, design and development of a B series propeller, hydrodynamic and structural performance analysis in uniform flow and free vibration test both in dry and wet condition. In order to perform the hydro-elastic based fluid structure interaction (FSI), Co-Simulation method was adopted to couple Reynolds Averaged Navier-Strokes Equation (RANSE) based Computational Fluid Dynamics (CFD) solver
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