Relevant bibliographies by topics / Transition laminaire turbulente

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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 'Transition laminaire turbulente'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Transition laminaire turbulente"

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Wesfreid, José Eduardo. "La tour Eiffel : le premier laboratoire d’aérodynamique en France." Reflets de la physique, no. 65 (April 2020): 30–33. http://dx.doi.org/10.1051/refdp/202065030.

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Cet article décrit sommairement la recherche expérimentale de Gustave Eiffel, qui a mis en évidence la forte réduction de la trainée d’une sphère dans un écoulement à grande vitesse, accompagnant le changement occasionné par la transition de la couche limite du corps depuis l’état laminaire vers l’état turbulent (crise de trainée). Cette découverte, mise en question initialement par Ludwig Prandtl, a été rendue possible par la conception et la réalisation par Eiffel d’un ensemble de nouvelles expériences astucieuses et de techniques innovantes créées autour de la tour Eiffel. Un siècle après l
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Volkov, V. E. "Mathematical simulation of laminar-turbulent transition and the turbulence scale estimation." Odes’kyi Politechnichnyi Universytet. Pratsi, no. 2 (December 15, 2014): 155–59. http://dx.doi.org/10.15276/opu.2.44.2014.27.

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Xu, Guoliang, and Song Fu. "A Four-Equation Eddy-Viscosity Approach for Modeling Bypass Transition." Advances in Applied Mathematics and Mechanics 6, no. 4 (2014): 523–38. http://dx.doi.org/10.4208/aamm.2013.m266.

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AbstractIt is very important to predict the bypass transition in the simulation of flows through turbomachinery. This paper presents a four-equation eddy-viscosity turbulence transition model for prediction of bypass transition. It is based on the SST turbulence model and the laminar kinetic energy concept. A transport equation for the non-turbulent viscosity is proposed to predict the development of the laminar kinetic energy in the pre-transitional boundary layer flow which has been observed in experiments. The turbulence breakdown process is then captured with an intermittency transport equ
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Marxen, Olaf, and Tamer A. Zaki. "Turbulence in intermittent transitional boundary layers and in turbulence spots." Journal of Fluid Mechanics 860 (December 5, 2018): 350–83. http://dx.doi.org/10.1017/jfm.2018.822.

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Direct numerical simulation data of bypass transition in flat-plate boundary layers are analysed to examine the characteristics of turbulence in the transitional regime. When intermittency is 50 % or less, the flow features a juxtaposition of turbulence spots surrounded by streaky laminar regions. Conditionally averaged turbulence statistics are evaluated within the spots, and are compared to standard time averaging in both the transition region and in fully turbulent boundary layers. The turbulent-conditioned root-mean-square levels of the streamwise velocity perturbations are notably elevate
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van Oudheusden, B. W. "An experimental study of transition and the development of turbulence in a linearly retarded boundary-layer flow." Aeronautical Journal 103, no. 1029 (1999): 497–510. http://dx.doi.org/10.1017/s0001924000064253.

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AbstractAn experimental investigation was carried out of the incompressible boundary layer flow along a flat plate, in the presence of an adverse pressure gradient that corresponds to a linear retardation of the free stream velocity. The turbulence level in the free-stream was 0·12% and transition occurred with the laminar boundary layer being close to separation. For three values of the Reynolds number (2·56, 3·11 and 4·09 million based on the reference length that is defined as the reciprocal of the nondimensional-velocity gradient) the laminar, transitional and turbulent regions were studie
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Steelant, J., and E. Dick. "Modeling of Laminar-Turbulent Transition for High Freestream Turbulence." Journal of Fluids Engineering 123, no. 1 (2000): 22–30. http://dx.doi.org/10.1115/1.1340623.

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To simulate transitional skin friction or heat transfer, the conditionally averaged Navier-Stokes equations are used. To describe the diffusion of freestream turbulence into the boundary layer and the intermittent laminar-turbulent flow behavior during transition, a turbulence weighting factor τ is used. A transport equation is presented for this τ-factor including convection, diffusion, production, and sink terms. In combination with the conditioned Navier-Stokes equations, this leads to an accurate calculation of flow characteristics within the transitional layer. The method is validated on
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Wang, T., T. W. Simon, and J. Buddhavarapu. "Heat Transfer and Fluid Mechanics Measurements in Transitional Boundary Layer Flows." Journal of Engineering for Gas Turbines and Power 107, no. 4 (1985): 1007–15. http://dx.doi.org/10.1115/1.3239804.

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Experimental results are presented to document hydrodynamic and thermal development of flat-plate boundary layers undergoing natural transition. Local heat transfer coefficients, skin friction coefficients, and profiles of velocity, temperature, and Reynolds normal and shear stresses are presented. A case with no transition and transitional cases with 0.68 percent and 2.0 percent free-stream disturbance intensities were investigated. The locations of transition are consistent with earlier data. A late-laminar state with significant levels of turbulence is documented. In late-transitional and e
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Blair, M. F. "Boundary-Layer Transition in Accelerating Flows With Intense Freestream Turbulence: Part 2—The Zone of Intermittent Turbulence." Journal of Fluids Engineering 114, no. 3 (1992): 322–32. http://dx.doi.org/10.1115/1.2910033.

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Hot-wire anemometry was employed to examine the laminar-to-turbulent transition of low-speed, two-dimensional boundary layers for two (moderate) levels of flow acceleration and various levels of grid-generated freestream turbulence. Flows with an adiabatic wall and with uniform-flux heat transfer were explored. Conditional discrimination techniques were employed to examine the zones of flow within the transitional region. This analysis demonstrated that as much as one-half of the streamwise-component unsteadiness, and much of the apparent anisotropy, observed near the wall was produced, not by
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Taghavi-Zenouz, R., M. Salari та M. Etemadi. "Prediction of laminar, transitional and turbulent flow regimes, based on three-equation k-ω turbulence model". Aeronautical Journal 112, № 1134 (2008): 469–76. http://dx.doi.org/10.1017/s0001924000002438.

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Abstract A recently developed transitional model for boundary-layer flows has been examined on a flat plate and the well-known S809 wind turbine blade. Proposed numerical model tries to simulate streamwise fluctuations, induced by freestream turbulence, in pre-transitional boundary-layer flows by introducing an additional transport equation for laminar kinetic energy term. This new approach can be used for modeling of transitional flows which are exposed to both the freestream turbulence intensity and streamwise pressure gradient, which are known as the most dominant factors in occurrence of t
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Schuster, Jean Jonathan, Cristiano Henrique Schuster, Eduardo Stüker, Áttila Leães Rodrigues, Luiz Eduardo Medeiros, and Felipe Denardin Costa. "OCORRÊNCIA DE INTERMITÊNCIA NA TRANSIÇÃO LAMINAR-TURBULENTA EM UM ESCOAMENTO DE COUETTE PLANO." Ciência e Natura 38 (July 20, 2016): 354. http://dx.doi.org/10.5902/2179460x20258.

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The transition from laminar-turbulent flow regime is important in most of the fluid mechanics application areas. In the planetary boundary layer (PBL), the flow is predominantly turbulent. However, shortly after sunset, the incidence of solar radiation ceases and the surface begins to lose heat through the emission of long-wave, yielding in a thermical stratified stable boundary layer (SBL), where turbulence can be suppressed in almost all scales. Under these conditions the production of turbulence is predominantly mechanical, and at nights with strong stratification, the turbulent activity is
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Dissertations / Theses on the topic "Transition laminaire turbulente"

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Baina, Samira. "Écoulement entre deux disques : instabilités et transition laminaire turbulent." Vandoeuvre-les-Nancy, INPL, 1994. http://www.theses.fr/1994INPL133N.

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Cette thèse est consacrée à l'étude expérimentale de la stabilité de l'écoulement entre deux disques dont l'un au moins est en rotation. L’instabilité qui apparait dans cette configuration est du type inflexionnel, elle est due à l'existence d'un point d'inflexion dans le profil de vitesse radiale. Dans une première partie, il s'agit d'étudier l'écoulement de base et d'établir les profils de vitesse correspondants. Ensuite une étude expérimentale a été entreprise grâce à la technique polarographique qui permet la mesure du gradient pariétal de vitesse. Cette étude a permis de mettre en évidenc
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Bernardos, Barreda Luis Francisco. "Modélisation de la transition vers la turbulence d'une couche limite décollée Algebraic Nonlocal Transition Modeling of Laminar Separation Bubbles Using k−ω Turbulence Models Prediction of Separation-Induced Transition on the SD7003 Airfoil Using Algebraic Transition Triggering". Thesis, Sorbonne université, 2019. http://www.theses.fr/2019SORUS184.

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Le but de cette thèse est de proposer des modèles qui améliorent la précision des prévisions RANS des bulbes de décollement laminaire. Dans un premier temps, des données de simulations numériques "haute-fidélité'' sur une configuration de référence ont été exploitées afin de comprendre les défauts des modèles existants. À partir de cette analyse, deux problèmes majeurs ont été mis en évidence : les modèles existants ne produisent pas de turbulence à un rythme suffisamment élevé dans la région transitionnelle décollée, et en général ils manquent de diffusivité dans la région située juste en ava
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Braza, Marianna. "Analyse physique du comportement dynamique d'un écoulement externe, décollé, instationnaire en transition laminaire-turbulente : application : cylindre circulaire." Toulouse, INPT, 1986. http://www.theses.fr/1986INPT057H.

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Braza, Marianna. "Analyse physique du comportement dynamique d'un écoulement externe, décolle, instationnaire en transition laminaire-turbulente application, cylindre circulaire." Grenoble 2 : ANRT, 1986. http://catalogue.bnf.fr/ark:/12148/cb375964149.

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Rolland, Joran. "Etude numérique à petite et grande échelle de la bande laminaire-turbulente de l'écoulement de Couette plan transitionnel." Phd thesis, Ecole Polytechnique X, 2012. http://pastel.archives-ouvertes.fr/pastel-00755414.

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La thèse propose une étude numérique et une modélisation de la transition vers la turbulence dans l'écoulement de Couette plan. On se concentre particulièrement sur le régime de bandes oblique laminaire turbulentes, au coeur de la transition. On suit deux types d'approches selon le type d'échelles considérées. D'une part on étudie le détail à petite échelle de l'écoulement. A l'aide de DNS, une instabilité de cisaillement créant de la vorticité transverse est mise en évidence, et la vitesse d'advection des perturbations est mesurée. La modélisation de l'écoulement turbulent et cette instabilit
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Persillon, Hélène. "Analyse physique par simulation numérique bi- et tri-dimensionnelle de la transition laminaire-turbulente dans l'écoulement autour d'un cylindre." Toulouse, INPT, 1995. http://www.theses.fr/1995INPT100H.

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Les equations de navier-stokes tridimensionnelles ont ete resolues pour predeterminer l'ecoulement derriere un cylindre circulaire. Les caracteristiques dynamiques de cette simulation ont ete comparees a celles issues du calcul bidimensionnel et ont permis de faire apparaitre la bifurcation tridimensionnelle ainsi que des nouvelles structures (tourbillons longitudinaux et transversaux). Les discontinuites observees experimentalement dans la relation du nombre de strouhal en fonction du nombre de reynolds ont ete simulees et expliquees. L'etude spectrale du sillage et l'evolution spatiale de l'
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Lefort, Eric. "Caractérisation des bifurcations et de la dynamique d'une lentille thermique par analyse spectrale." Rouen, 1987. http://www.theses.fr/1987ROUES019.

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Un faisceau laser est focalisé sur la face d'entrée d'une cuve transparente remplie d'un liquide absorbant. Une lentille thermique est formée; les oscillations de la lentille sont la manifestation visible d'oscillations hydrodynamiques du liquide dans la cuve. Le système présente un comportement de transition laminaire turbulente, un certain nombre de bifurcations ayant été observées. Analyse spectrale du signal temporel
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Laurent, Célia. "Étude d'écoulements transitionnels et hors équilibre par des approches DNS et RANS." Phd thesis, Paris, ENSAM, 2012. http://pastel.archives-ouvertes.fr/pastel-00834850.

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Le décrochage est un phénomène aérodynamique instationnaire susceptible d'apparaître sur de nombreux profils aérodynamiques. Il résulte d'un décollement important de l'écoulement vis-à-vis de la paroi de l'aile et dégrade considérablement les performances de vol. Sur certains profils de pales d'hélicoptères, d'éoliennes ou de rotors, ce phénomène se produit dans des conditions d'utilisation normales et justifie la recherche de méthodes de modélisation accessibles industriellement. Le décrochage est initié au bord d'attaque par l'apparition d'une petite région de recirculation de fluide appelée
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Gross, Raphaël. "Prise en compte de la transition laminaire / turbulent dans un code Navier-Stokes éléments finis non structurés." Thesis, Toulouse, ISAE, 2015. http://www.theses.fr/2015ESAE0022/document.

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La thèse vise à intégrer des critères de transition dans le solveur Navier-Stokes non structuré Aether utilisé chez Dassault Aviation. Une méthodologie de prévision de la transition laminaire/turbulent a été élaborée et implémentée dans le solveur RANS Aether. Deux stratégies de calcul de transition ont été testées. Soit Aether est couplé avec le code de couche limite de l’ONERA 3C3D. Soit la position de transition est calculée en utilisant directement les profils de vitesse RANS. Les deux méthodes ont été testées pour des écoulements subsoniques et transsoniques. L’influence des solveurs numé
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Chiffaudel, Arnaud. "Dynamique spatio-temporelle de la convection a bas nombre de prandtl." Paris 7, 1988. http://www.theses.fr/1988PA077037.

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Etude experimentale de la convection de rayleigh-benard. Description et caracterisation des regimes dynamiques successifs de l'etat stationnaire a l'etat turbulent dans le cadre de theories faiblement non-lineaires
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Books on the topic "Transition laminaire turbulente"

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Kozlov, V. V., ed. Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1985. http://dx.doi.org/10.1007/978-3-642-82462-3.

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Fasel, Hermann F., and William S. Saric, eds. Laminar-Turbulent Transition. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-03997-7.

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Kobayashi, Ryoji, ed. Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1995. http://dx.doi.org/10.1007/978-3-642-79765-1.

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Arnal, D., and R. Michel, eds. Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3.

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Sherwin, Spencer, Peter Schmid, and Xuesong Wu, eds. IUTAM Laminar-Turbulent Transition. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-030-67902-6.

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Govindarajan, Rama, ed. IUTAM Symposium on Laminar-Turbulent Transition. Springer Netherlands, 2006. http://dx.doi.org/10.1007/1-4020-4159-4.

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Wagner, Siegfried, Markus Kloker, and Ulrich Rist, eds. Recent Results in Laminar-Turbulent Transition. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-540-45060-3.

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Schlatter, Philipp, and Dan S. Henningson, eds. Seventh IUTAM Symposium on Laminar-Turbulent Transition. Springer Netherlands, 2010. http://dx.doi.org/10.1007/978-90-481-3723-7.

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Innes, Graeme E. Laminar-to-turbulent transition in tilting-pad bearings. s.n.], 1989.

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IUTAM Symposium on Laminar-Turbulent Transition (5th 1999 Sedona, Arizona). Laminar-turbulent transition: IUTAM Symposium, Sedona/USA, 1999. Springer, 2000.

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Book chapters on the topic "Transition laminaire turbulente"

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Hirschel, Ernst Heinrich, Jean Cousteix, and Wilhelm Kordulla. "Laminar-Turbulent Transition and Turbulence." In Three-Dimensional Attached Viscous Flow. Springer Berlin Heidelberg, 2014. http://dx.doi.org/10.1007/978-3-642-41378-0_9.

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Schobeiri, Meinhard T. "Laminar-Turbulent Transition." In Fluid Mechanics for Engineers. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-11594-3_8.

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Morkovin, M. V., and E. Reshotko. "Dialogue on Progress and Issues in Stability and Transition Research." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_1.

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Carpenter, P. W., and P. K. Sen. "Effects of Boundary-Layer Growth on the Linear Regime of Transition over Compliant Walls." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_10.

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Nitsche, W., P. Mirow, and T. Dörfler. "Investigations on Flow Instabilities on Airfoils by Means of Piezofoil-Arrays." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_11.

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Zelman, M. B., and I. I. Maslennikova. "On the Spatial Structure of Disturbances in Boundary Layer Subharmonic Transition." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_12.

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Stewart, P. A. "Three-Dimensional Effects in Boundary-Layer Transition: A High Reynolds Number Weakly-Nonlinear Theory." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_13.

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Corke, T. C. "Effect of Controlled Resonant Interactions and Mode Detuning on Turbulent Transition in Boundary Layers." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_14.

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Landahl, Marten T. "Role of Transients in Boundary Layer Instability and Transition." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_15.

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Breuer, Kenneth S. "The Evolution of a Localized Disturbance in a Laminar Boundary Layer." In Laminar-Turbulent Transition. Springer Berlin Heidelberg, 1990. http://dx.doi.org/10.1007/978-3-642-84103-3_16.

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Conference papers on the topic "Transition laminaire turbulente"

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Steelant, J. "Modelling of laminar-turbulent transition for high free-stream turbulence." In 30th Fluid Dynamics Conference. American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-3790.

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Lopez, Maurin, and D. K. Walters. "Laminar-to-Turbulent Boundary Layer Prediction Using an Alternative to the Laminar Kinetic Energy Approach." In ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-89433.

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This paper presents a new model concept for prediction of boundary layer transition using a linear eddy-viscosity RANS approach. It is a single-point, physics-based method that adopts an alternative to the Laminar Kinetic Energy (LKE) framework. The model is based on a description of the transition process previously discussed by Walters (2009). The version of the model presented here uses the k-ω SST model as the baseline, and includes the effects of transition through one additional transport equation for v2. Here v2 is interpreted as the energy of fully turbulent, 3D velocity fluctuations,
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Lukashev, E. A., E. V. Radkevich, N. N. Yakovlev, and O. A. Vasil’eva. "On laminar-turbulent transition." In APPLICATIONS OF MATHEMATICS IN ENGINEERING AND ECONOMICS (AMEE’16): Proceedings of the 42nd International Conference on Applications of Mathematics in Engineering and Economics. Author(s), 2016. http://dx.doi.org/10.1063/1.4968432.

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Fasihfar, Ahmad, and Mark W. Johnson. "An Improved Boundary Layer Transition Correlation." 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-245.

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The influence of pressure gradient and freestream turbulence level on boundary layer transition has been studied experimentally using hot wire instrumentation and digital signal processing and analysis. An established transition correlation and recent transition model were found to give acceptable prediction of the experimental results. The digital system was used to conditionally sample the transitional boundary layer data and hence to determine the mean and fluctuating velocity profiles for the laminar and turbulent parts of the boundary layer separately. The turbulent portions were found to
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Gostelow, J. P., G. Hong, G. J. Walker, and J. Dey. "Modeling of Boundary Layer Transition in Turbulent Flows by Linear Combination Integral Method." In ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1994. http://dx.doi.org/10.1115/94-gt-358.

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Transitional boundary layer parameters in zero and variable pressure gradient flows, typical of turbomachinery applications, are predicted using an integral method of the linear combination type. The code used is that of Dey and Narasimha and the turbulent layer is calculated by a lag-entrainment method. The predictions of test data represent an improvement upon earlier methods; although reasonable agreement is obtained for these low Reynolds number test cases further refinement of predictive correlations to account for free-stream turbulence effects on laminar boundary layers and transition i
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Yershov, Sergiy, and Viktor Yakovlev. "Validation of the PTM Transition Model on a 3D Flow Through a Turbine Cascade." In ASME 2016 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2016. http://dx.doi.org/10.1115/imece2016-65001.

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This study presents a numerical simulation of a 3D viscous subsonic flow in the VKI-Genoa turbine cascade taking into account the laminar-turbulent transition. The numerical simulation is performed using the Reynolds-averaged Navier-Stokes (RANS) equations and the low-Reynolds k-ω SST turbulence model. The Langtry’s algebraic Production Term Modification (PTM) model is applied for modeling the laminar-turbulent transition. The governing equations are integrated using the second-order accurate Godunov’s type implicit ENO scheme. Computations of both fully turbulent and transitional flows are ca
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Mayle, Robert Edward. "The Role of Laminar-Turbulent Transition in Gas Turbine Engines." In ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1991. http://dx.doi.org/10.1115/91-gt-261.

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A critical study of laminar-turbulent transition phenomena and its role in aerodynamics and heat transfer in modern and future gas turbine engines is presented. In order to develop a coherent view of the subject, a current look at transition phenomena from both a theoretical and experimental standpoint are provided and a comprehensive state-of-the-art account of transitional phenomena in the engine’s throughflow components given. The impact of transitional flow on engine design is discussed and suggestions for future research and developmental work provided.
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Bader, Pascal, and Wolfgang Sanz. "On Boundary Layer Relaminarization in an Highly Accelerated High Pressure Turbine Stator Flow." In ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gt2017-63296.

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The boundary layer represents the thin layer between the wall and the free stream. Although this zone is small in respect to the free stream its state — whether it is laminar or turbulent — has a high impact on wall parameters like skin friction but also on the free stream. The state of the boundary layer is influenced by free stream parameters like free stream turbulence intensity or acceleration. Transition can occur from laminar to turbulent, but also from turbulent to laminar. The latter process is called relaminarization. Transition and relaminarization has already been detected in labora
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Stripf, M., A. Schulz, and H. J. Bauer. "Modeling of Rough Wall Boundary Layer Transition and Heat Transfer on Turbine Airfoils." In ASME Turbo Expo 2006: Power for Land, Sea, and Air. ASMEDC, 2006. http://dx.doi.org/10.1115/gt2006-90316.

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A new model for predicting heat transfer in the transitional boundary layer of rough turbine airfoils is presented. The new model makes use of extensive experimental work recently published by the current authors. For the computation of the turbulent boundary layer a discrete element roughness model is combined with a two-layer model of turbulence. The transition region is modeled using an intermittency equation that blends between the laminar and turbulent boundary layer. Several intermittency functions are evaluated in respect of their applicability to rough-wall transition. To predict the o
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Matt, Silvia C., Weilin Hou, and Damien Josset. "Optical sensing of laminar to turbulent transition and boundary layer turbulence (Conference Presentation)." In Ocean Sensing and Monitoring XI, edited by Weilin "Will" Hou and Robert A. Arnone. SPIE, 2019. http://dx.doi.org/10.1117/12.2521321.

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Reports on the topic "Transition laminaire turbulente"

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Fasel, Hermann F. IUTAM Symposium: Laminar-Turbulent Transition. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada391139.

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Wagnild, Ross, Jeffrey Fike, Alec Kucala, Michael Krygier, and Neal Bitter. Coupling of Laminar-Turbulent Transition with RANS Computational Fluid Dynamics. Office of Scientific and Technical Information (OSTI), 2020. http://dx.doi.org/10.2172/1670532.

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Ferziger, Joel H., and Helen L. Reed. Simulation of Laminar-Turbulent Transition in the Vicinity of a Wall. Defense Technical Information Center, 1988. http://dx.doi.org/10.21236/ada191380.

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Weyburne, David W. New Shape Parameters for the Laminar, Transitional, and Turbulent Velocity Profiles. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada519321.

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Schneider, Steven P., and Steven H. Collicott. Laminar-Turbulent Transition in High-Speed Compressible Boundary Layers: Continuation of Elliptic-Cone Experiments. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada373478.

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Grossir, Guillaume. On the design of quiet hypersonic wind tunnels. Von Karman Institute for Fluid Dynamics, 2020. http://dx.doi.org/10.35294/tm57.

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This document presents a thorough literature review on the development of hypersonic quiet tunnels. The concept of boundary layer transition in high-speed flows is presented first. Its consequences on the free-stream turbulence levels in ground facilities are reviewed next, demonstrating that running boundary layers along the nozzle walls must remain laminar for quiet operation. The design key points that enable laminar boundary layers and hypersonic operation with low free-stream noise levels are then identified and discussed. The few quiet facilities currently operating through the world are
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SCHNEIDER, Steven P., and Steven H. Collicott. Laminar-Turbulent Transition in High-Speed Compressible Boundary Layers with Curvature: Non-Zero Angle of Attack Experiments. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada329733.

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