Relevant bibliographies by topics / Gaz compressibles

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  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Gaz compressibles'

Author: Grafiati
Published: 4 June 2021
Last updated: 3 February 2022

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Journal articles on the topic "Gaz compressibles"

1

Combe, Laure, and Jean-Marc Hérard. "Un schéma Volumes-Finis pour la simulation d'un modèle bi-fluide d'écoulements diphasiques compressibles gaz-solide." Revue Européenne des Éléments Finis 6, no. 2 (1997): 197–231. http://dx.doi.org/10.1080/12506559.1997.10511266.

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CAI, CHUNPEI, QUANHUA SUN, and IAIN D. BOYD. "Gas flows in microchannels and microtubes." Journal of Fluid Mechanics 589 (October 8, 2007): 305–14. http://dx.doi.org/10.1017/s0022112007008178.

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This study analyses compressible gas flows through microchannels or microtubes, and develops two complete sets of asymptotic solutions. It is a natural extension of the previous work by Arkilicet al. on compressible flows through microchannels. First, by comparing the magnitudes of different forces in the compressible gas flow, we obtain proper estimations for the Reynolds and Mach numbers at the outlets. Second, based on these estimations, we obtain asymptotic analytical solutions of velocities, pressure and temperature distributions of compressible gas flow inside the microchannels and micro
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Moore, J., and K. M. Elward. "Shock Formation in Overexpanded Tip Leakage Flow." Journal of Turbomachinery 115, no. 3 (1993): 392–99. http://dx.doi.org/10.1115/1.2929266.

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Shock formation due to overexpansion of supersonic flow at the inlet to the tip clearance gap of a turbomachine has been studied. The flow was modeled on a water table using a sharp-edged rectangular channel. The flow exhibited an oblique hydraulic jump starting on the channel sidewall near the channel entrance. This flow was analyzed using hydraulic theory. The results suggest a model for the formation of the jump. The hydraulic analogy between free surface water flows and compressible gas flows is used to predict the location and strength of oblique shocks in analogous tip leakage flows. Fea
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Blanc, Xavier, Raphaël Danchin, Bernard Ducomet, and Šárka Nečasová. "The global existence issue for the compressible Euler system with Poisson or Helmholtz couplings." Journal of Hyperbolic Differential Equations 18, no. 01 (2021): 169–93. http://dx.doi.org/10.1142/s0219891621500041.

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We consider the Cauchy problem for the barotropic Euler system coupled to Helmholtz or Poisson equations, in the whole space. We assume that the initial density is small enough, and that the initial velocity is close to some reference vector field [Formula: see text] such that the spectrum of [Formula: see text] is positive and bounded away from zero. We prove the existence of a global unique solution with (fractional) Sobolev regularity, and algebraic time decay estimates. Our work extends Grassin and Serre’s papers [Existence de solutions globales et régulières aux équations d’Euler pour un
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Welsh, Stephanie, Evy Kersalé, and Chris A. Jones. "Compressible Taylor–Couette flow – instability mechanism and codimension 3 points." Journal of Fluid Mechanics 750 (June 10, 2014): 555–77. http://dx.doi.org/10.1017/jfm.2014.279.

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AbstractTaylor–Couette flow in a compressible perfect gas is studied. The onset of instability is examined as a function of the Reynolds numbers of the inner and outer cylinder, the Mach number of the flow and the Prandtl number of the gas. We focus on the case of a wide gap, with radius ratio 0.5. We find new modes of instability at high Prandtl number, which can allow oscillatory axisymmetric modes to onset first. We also find that onset can occur even when the angular momentum increases outwards, so that the classical Rayleigh criterion can be violated in the compressible case. We have also
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GOPINATH, ARVIND, SHING B. CHEN, and DONALD L. KOCH. "Lubrication flows between spherical particles colliding in a compressible non-continuum gas." Journal of Fluid Mechanics 344 (August 10, 1997): 245–69. http://dx.doi.org/10.1017/s002211209700606x.

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The low-Reynolds-number collision and rebound of two rigid spheres moving in an ideal isothermal gas is studied in the lubrication limit. The spheres are non-Brownian in nature with radii much larger than the mean-free path of the molecules. The nature of the flow in the gap between the particles depends on the relative magnitudes of the minimum gap thickness, h′o, the mean-free path of the bulk gas molecules, λo, and the gap thickness at which compressibility effects become important, hc. Both the compressible nature of the gas and the non-continuum nature of the flow in the gap are included
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Matušů-Nečasová, Šárka. "Global solution of viscous compressible barotropic multipolar gas in a finite channel with nonzero input and output." Applications of Mathematics 37, no. 3 (1992): 161–71. http://dx.doi.org/10.21136/am.1992.104501.

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MANELA, A., and I. FRANKEL. "On the compressible Taylor–Couette problem." Journal of Fluid Mechanics 588 (September 24, 2007): 59–74. http://dx.doi.org/10.1017/s0022112007007422.

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We consider the linear temporal stability of a Couette flow of a Maxwell gas within the gap between a rotating inner cylinder and a concentric stationary outer cylinder both maintained at the same temperature. The neutral curve is obtained for arbitrary Mach (Ma) and arbitrarily small Knudsen (Kn) numbers by use of a ‘slip-flow’ continuum model and is verified via comparison to direct simulation Monte Carlo results. At subsonic rotation speeds we find, for the radial ratios considered here, that the neutral curve nearly coincides with the constant-Reynolds-number curve pertaining to the critic
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Liu, Jian, and Shi Qing Wang. "Weakly Compressible Fluid Model to Study Thermal Effects on Laser Propagating in Closed Tube." Advanced Materials Research 354-355 (October 2011): 165–69. http://dx.doi.org/10.4028/www.scientific.net/amr.354-355.165.

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Analyzed the iso-pressure approximate model used in laser propagation in gas medium and pointed out its disadvantage under complex border conditions. The weakly compressible fluid model was developed which was based on the Mach uniform method introduced by Peter Wesseling. Using the weakly compressible fluid model and scalar wave equation, a numerical study was carried out for the gas thermal effects on laser propagating in a closed tube full-filled with air. The far-field beam shape at different time were obtained and compared with the experiment ones. It is shown that the weakly compressible
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Feldman, Y., Y. Kligerman, and I. Etsion. "Stiffness and Efficiency Optimization of a Hydrostatic Laser Surface Textured Gas Seal." Journal of Tribology 129, no. 2 (2006): 407–10. http://dx.doi.org/10.1115/1.2540120.

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Microdimples generated by laser surface texturing (LST) can be used to enhance performance in hydrostatic gas-lubricated mechanical seals. This is achieved by applying microdimples with high area density over a certain portion of the sealing dam width adjacent to the high-pressure side, leaving the remaining portion untextured. The textured portion provides an equivalent larger gap that results in converging clearance in the direction of pressure drop and hence, hydrostatic pressure buildup, similar to that of a radial step seal. A mathematical model based on the solution of the Reynolds equat
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Dissertations / Theses on the topic "Gaz compressibles"

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Aubert, Cécile. "Ecoulements compressibles de gaz dans les microcanaux : effets de raréfaction, effets instationnaires." Toulouse 3, 1999. http://www.theses.fr/1999TOU30053.

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Cette etude concerne les ecoulements compressibles de gaz dans les microcanaux. Pour des pressions et temperatures usuelles, le nombre de knudsen est compris entre 0. 001 et 0. 1. L'ecoulement est de type glissant et peut etre modelise par les equations de navier-stokes associees a des conditions de vitesse de glissement et de saut de temperature a la paroi, generalement exprimees par les equations du premier ordre de maxwell-smoluchowski. Dans une premiere partie, une analyse de l'etat de l'art sur les microsystemes a fluides et sur l'etablissement des conditions aux limites est presentee. Da
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Bongiovanni, Emmanuel. "Méthodes de relaxation pour les équations de Navier-Stokes compressibles." Phd thesis, Ecole des Ponts ParisTech, 2002. http://tel.archives-ouvertes.fr/tel-00005676.

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On présente une nouvelle méthode de relaxation pour résoudre les équations de Navier-Stokes compressibles munies d'une loi de pression générale. La méthode s'inspire de la décomposition de l'énergie interne introduite par Coquel et Perthame (SIAM J. Numer. Anal., 35 (6), 2223-2249, 1998) pour les équations d'Euler. Elle conserve, en particulier, les mêmes conditions "sous-caractéristiques" pour l'exposant adiabatique du gaz fictif intervenant dans la relaxation. Dans cette thèse, on introduit une décomposition des flux diffusifs (tenseur des contraintes visqueuses et flux de chaleur) qui assur
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Benharbit, Saad Vila Jean-Paul. "Sur la théorie et l'approximation numérique des problèmes hyperboliques non linéaires application à la dynamique des gaz compressibles /." S.l. : Université Grenoble 1, 2008. http://tel.archives-ouvertes.fr/tel-00341589.

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Birolleau, Alexandre. "Résolution de problème inverse et propagation d'incertitudes : application à la dynamique des gaz compressibles." Phd thesis, Université Pierre et Marie Curie - Paris VI, 2014. http://tel.archives-ouvertes.fr/tel-01023856.

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Cette thèse porte sur la propagation d'incertitudes et la résolution de problème inverse et leur accélération par Chaos Polynomial. L'objectif est de faire un état de l'art et une analyse numérique des méthodes spectrales de type Chaos Polynomial, d'en comprendre les avantages et les inconvénients afin de l'appliquer à l'étude probabiliste d'instabilités hydrodynamiques dans des expériences de tubes à choc de type Richtmyer-Meshkov. Le second chapitre fait un état de l'art illustré sur plusieurs exemples des méthodes de type Chaos Polynomial. Nous y effectuons son analyse numérique et mettons
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Rouy, Sandra. "Modélisation mathématique et numérique d'écoulements diphasiques compressibles : application au cas industriel d'un générateur de gaz." Toulon, 2000. http://www.theses.fr/2000TOUL0004.

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Sart, Rémy. "Etude de problèmes liés aux fluides compressibles et aux plasmas." Phd thesis, Université Blaise Pascal - Clermont-Ferrand II, 2007. http://tel.archives-ouvertes.fr/tel-00211826.

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Mes études portent sur des questions de stabilité pour différents modèles compressibles et magnétiques.<br /><br />Tout d'abord, je me suis intéressé aux généralisations magnétiques possibles de quelques résultats pour Navier-Stokes compressible.<br />La prise en compte de la viscosité est cruciale et peut faire l'objet de diverses hypothèses, en particulier, des profils constants ou dépendants des caractéristiques du fluide conditionnent le caractère bien posé des modèles compressibles.<br />Les résultats proposés apportent une contribution aux études complexes de la MHD, notamment sur les qu
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Benharbit, Saad. "Sur la théorie et l'approximation numérique des problèmes hyperboliques non linéaires :." Phd thesis, Grenoble 1, 1992. http://tel.archives-ouvertes.fr/tel-00341589.

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Dans ce travail de thèse sont étudiés des problèmes mathématiques (théorie et approximation) issus de la théorie de la dynamique des gaz compressibles et modélisés par les équations d'Euler. L'approximation numérique de ces problèmes physiques a nécessite une étude détaillée de quelques problèmes de conditions aux limites. Les approximations numériques obtenues sont basées sur la methode des volumes finis, qui nous a semble la mieux adaptée pour la discrétisation des systèmes hyperboliques de lois de conservation en général. La convergence de la methode des volumes finis est obtenue pour les p
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Hank, Sarah. "Modélisation et simulation de la dispersion de fluide en milieu fortement hétérogène." Thesis, Aix-Marseille, 2012. http://www.theses.fr/2012AIXM4765/document.

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Ces travaux portent sur la modélisation et la simulation numérique de la dispersion de matériaux nocifs (pulvérisations liquides ou gazeuses) en milieu urbain ou naturel (attentat ou explosion accidentelle survenant en zone peuplée, fuites de produits toxiques gazeux ou liquides, éclatement de réservoir..). Afin de prédire ces risques un outils de simulation tridimensionnel a été développé. Celui-ci est basé sur un modèle de milieu hétérogène afin de traiter des phénomènes dont la durée et les distances associées peuvent être très grandes. La topographie des milieux étudiées est prise en compt
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Rabie, François. "Programmation et validation d'un code d'éléments finis 2D quadrangulaires pour une formulation lagrangienne des équations de la dynamique des gaz compressibles en régime instationnaire avec implantation d'un remaillage d'ordre 2." Grenoble 2 : ANRT, 1988. http://catalogue.bnf.fr/ark:/12148/cb376177873.

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Rabie, François. "Programmation et validation d'un code d'elements finis 2d quadrangulaires pour une formulation lagrangienne des equations de la dynamique des gaz compressibles en regime instationnaire, avec implantation d'un remaillage d'ordre 2." Paris 6, 1988. http://www.theses.fr/1988PA066501.

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Books on the topic "Gaz compressibles"

1

Yahya, S. M. Gas tables for compressible flow calculations. 5th ed. New Age International (P) Ltd., Publishers, 2006.

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2

Modern compressible flow: With historical perspective. 3rd ed. McGraw-Hill, 2003.

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Modern compressible flow: With historical perspective. 2nd ed. McGraw-Hill, 1990.

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Délery, J. Handbook of compressible aerodynamics. ISTE, 2010.

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Handbook of compressible aerodynamics. ISTE, 2010.

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Wang, B. Y. Compressible laminar boundary-layer flows of a dusty gas over a semi-infinite flat plate. [s.n.], 1988.

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Husain, Zoeb. Compressible flow through problems or gas dynamics through problems. Wiley, 1989.

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Perthame, B. On positively preserving finite volume schemes for compressible Euler Equations. National Aeronautics and Space Administration, Langley Research Center, 1993.

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Perthame, Benoit. On positively preserving finite volume schemes for compressible Euler Equations. National Aeronautics and Space Administration, Langley Research Center, 1993.

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Roe, P. L. Remote boundary conditions for unsteady multidimensional aerodynamic computations. National Aeronautics and Space Administration, Langley Research Center, 1987.

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Book chapters on the topic "Gaz compressibles"

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Després, Bruno. "Le système de la dynamique des gaz compressibles." In Lois de Conservations Eulériennes, Lagrangiennes et Méthodes Numériques. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-11657-5_5.

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Achterberg, Abraham. "Steady, Ideal Compressible Flows." In Gas Dynamics. Atlantis Press, 2016. http://dx.doi.org/10.2991/978-94-6239-195-6_6.

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Sasoh, Akihiro. "Motion of Gas Particles and Thermodynamics." In Compressible Fluid Dynamics and Shock Waves. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-0504-1_2.

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Cassady, P. E., S. F. Birch, and P. J. Terry. "Aero-Optical Analysis of a Compressible Shear Layer." In Gas Flow and Chemical Lasers. Springer Berlin Heidelberg, 1987. http://dx.doi.org/10.1007/978-3-642-71859-5_56.

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Li, Dang, and Junbin Chen. "Unsteady Percolation of Slightly Compressible Fluid." In Mechanics of Oil and Gas Flow in Porous Media. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-7313-2_4.

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Bryant, Michael D. "Reynolds Equation for Compressible Fluid or Gas Film." In Encyclopedia of Tribology. Springer US, 2013. http://dx.doi.org/10.1007/978-0-387-92897-5_223.

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Shyue, Keh-Ming. "An Eulerian Interface-Sharpening Algorithm for Compressible Gas Dynamics." In Modeling, Simulation and Optimization of Complex Processes - HPSC 2012. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-09063-4_18.

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Paskonov, V. M., and M. S. Artamonova. "Numerical Simulation of Separated Unsteady Flows of Viscous Compressible Gas." In Separated Flows and Jets. Springer Berlin Heidelberg, 1991. http://dx.doi.org/10.1007/978-3-642-84447-8_57.

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Sciacovelli, L., P. Cinnella, and X. Gloerfelt. "Analysis of Dense Gas Effects in Compressible Turbulent Channel Flows." In Direct and Large-Eddy Simulation XI. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-04915-7_45.

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Després, Bruno, and Emmanuel Labourasse. "Towards stabilization of cell-centered Lagrangian methods for compressible gas dynamics." In Finite Volumes for Complex Applications VI Problems & Perspectives. Springer Berlin Heidelberg, 2011. http://dx.doi.org/10.1007/978-3-642-20671-9_34.

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Conference papers on the topic "Gaz compressibles"

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Jaiswal, Abhijeet, Ashwin S. Dhoble, and D. J. Tidke. "High Compressible Flow Through Jet Blast Deflector." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4699.

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Jet blast impact on aerofoil blade of the deflector is studied which redirects the high energy exhaust of jet engine during the ground testing. The geometric model of aerofoils is designed with structured mesh around the aerofoil in rectangular domain generated in ICEM 16 software. The jet blast impact on aerofoil blade of the deflector is numerically simulated with SST k-ω model based on CFD theory. The fluid flow is high-speed compressible flow and flowing fluid air is considered as an ideal gas and also Sutherland’s law viscosity is applied to account for the dependence of molecular viscosi
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Power, G. D., J. M. Verdon, and K. A. Kousen. "Analysis of Unsteady Compressible Viscous Layers." In ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1990. http://dx.doi.org/10.1115/90-gt-014.

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The development of an analysis to predict the unsteady compressible flows in blade boundary layers and wakes is presented. The equations that govern the flows in these regions are transformed using an unsteady turbulent generalization of the Levy-Lees transformation. The transformed equations are solved using a finite difference technique in which the solution proceeds by marching in time and in the streamwise direction. Both laminar and turbulent flows are studied, the latter using algebraic turbulence and transition models. Laminar solutions for a flat plate are shown to approach classical a
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Ohwada, Taku. "Boltzmann schemes for the compressible Navier-Stokes equations." In RAREFIED GAS DYNAMICS: 22nd International Symposium. AIP, 2001. http://dx.doi.org/10.1063/1.1407578.

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Skovorodko, P. A. "Slip effects in compressible turbulent channel flow." In 28TH INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS 2012. AIP, 2012. http://dx.doi.org/10.1063/1.4769570.

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Jain, V., and C. Lin. "Three-Dimensional Compressible Gas Flow in Microchannnels." In 44th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-1423.

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Sielemann, Michael. "High-Speed Compressible Flow and Gas Dynamics." In 9th International MODELICA Conference, Munich, Germany. Linköping University Electronic Press, 2012. http://dx.doi.org/10.3384/ecp1207681.

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Zeidan, D., A. Slaouti, and R. Touma. "Compressible gas-solid mixture conservation laws simulations." In NUMERICAL ANALYSIS AND APPLIED MATHEMATICS ICNAAM 2012: International Conference of Numerical Analysis and Applied Mathematics. AIP, 2012. http://dx.doi.org/10.1063/1.4756088.

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Kustova, E. V., E. A. Nagnibeda, D. Giordano, and Takashi Abe. "Chemical-Reaction Rates in Non-equilibrium Viscous Compressible Flows." In RARIFIED GAS DYNAMICS: Proceedings of the 26th International Symposium on Rarified Gas Dynamics. AIP, 2008. http://dx.doi.org/10.1063/1.3076584.

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Abou-Haidar, N. I., and S. L. Dixon. "Compressible Flow Pressure Losses in Wye-Junctions." In ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1992. http://dx.doi.org/10.1115/92-gt-071.

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This paper considers the compressible flow pressure losses in sharp cornered wye-junctions with symmetrical branches under dividing and combining flow conditions. Determination of the additional total pressure losses occurring in flow through several three-leg junctions, using dry air as the working fluid, has been made experimentally. Results covering a wide speed range up to choking are presented for three different wye-junction geometries. Separate flow visualisation Schlieren tests detected the presence of normal shock waves, located at up to one duct diameter downstream of the junction, a
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Wilson, D. E. "An Explicit Inverse Design Formulation for Compressible Flow." In ASME 1986 International Gas Turbine Conference and Exhibit. American Society of Mechanical Engineers, 1986. http://dx.doi.org/10.1115/86-gt-81.

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A new singular integral equation method has been developed for solving the full nonlinear potential flow about an arbitrary body. The method bears some resemblance to conventional integral methods, however it is inherently different in that the surface geometry is contained explicitly in the resulting integral equations. Several analytical results are exploited to reduce the two-dimensional integral equations to a one-dimensional problem on the body surface. The integral equation is inverted so that the airfoil geometry is given as an explicit function of the velocity field. The resulting one-
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Reports on the topic "Gaz compressibles"

1

Suo-Anttila, A. F2D users manual: A two-dimensional compressible gas flow code. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/10188561.

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Roy S. Baty, F. Farassat, John A. Hargreaves. Nonstandard Analysis and Shock Wave Jump Conditions in a One-Dimensional Compressible Gas. Office of Scientific and Technical Information (OSTI), 2007. http://dx.doi.org/10.2172/913104.

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