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Relevant bibliographies by topics / Mixing planes

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Academic literature on the topic 'Mixing planes'

Author: Grafiati

Published: 10 March 2023

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Journal articles on the topic "Mixing planes"

1

Juraeva, Makhsuda, and Dong Jin Kang. "Mixing Performance of a Cross-Channel Split-and-Recombine Micro-Mixer Combined with Mixing Cell." Micromachines 11, no. 7 (2020): 685. http://dx.doi.org/10.3390/mi11070685.

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A new cross-channel split-and-recombine (CC-SAR) micro-mixer was proposed, and its performance was demonstrated numerically. A numerical study was carried out over a wide range of volume flow rates from 3.1 μL/min to 826.8 μL/min. The corresponding Reynolds number ranges from 0.3 to 80. The present micro-mixer consists of four mixing units. Each mixing unit is constructed by combining one split-and-recombine (SAR) unit with a mixing cell. The mixing performance was analyzed in terms of the degree of mixing and relative mixing cost. All numerical results show that the present micro-mixer perfor

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Zazymko, V. O., M. F. Kalinina, V. Y. Shibetsky, and O. M. Nedbailo. "Hydrodynamics of a reactor with updated structure of frame mixing device." Кераміка: наука і життя, no. 3(52) (September 30, 2021): 7–14. http://dx.doi.org/10.26909/csl.3.2021.1.

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This article is devoted to computer simulation of the hydrodynamic situation in a reactor with a standard design and an upgraded design of a frame stirrer. A comparative analysis of the hydrodynamics of fluid flows occurring in the volume due to the use of classical and modernized design was performed. An upgraded design of a frame stirrer for homogenizing the medium in a reactor has been proposed. The aim of this work was to study the influence of the geometry of the stirrer blades and their location in space on the speed and direction of flows in the reactor. The basis for the ne

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Robens, Tania. "Two-Real-Singlet-Model Benchmark Planes." Symmetry 15, no. 1 (2022): 27. http://dx.doi.org/10.3390/sym15010027.

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In this manuscript, I briefly review the Benchmark Planes in the Two-Real-Singlet Model (TRSM), a model that enhances the Standard Model (SM) scalar sector by two real singlets that obey a Z2⊗Z2′ symmetry. In this model, all fields acquire a vacuum expectation value, such that the model contains in total three CP-even neutral scalars that can interact with each other. All interactions with SM-like particles are inherited from the SM-like doublet via mixing. I remind the readers of the previously proposed benchmark planes and briefly discuss possible production at future Higgs factories, as wel

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Andrievschi, Serghei, Valeriu Lungu, Ala Carcea, and Alexandru Lozan. "The Quality of Mixing in Mixers with Bars and Radial and Longitudinal Scrapers." Romanian Journal of Transport Infrastructure 2, no. 1 (2013): 10–20. http://dx.doi.org/10.1515/rjti-2015-0008.

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Abstract The process of division - combining of streams in mixers with bars and radial and longitudinal scrapers was studied. The number of unique streams that are formed after passing each row of longitudinal bars and the total amount of them were determined. This is demonstrated by migration of the particles along the mixer from left to right and vice versa, from the center of the drum towards the periphery and vice versa. In the process of mixing the particles in the center gain normal distribution and the ones on the side - sectioned normal distribution. The sum of normal distribution with

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5

Dawes, W. N. "Toward Improved Throughflow Capability: The Use of Three-Dimensional Viscous Flow Solvers in a Multistage Environment." Journal of Turbomachinery 114, no. 1 (1992): 8–17. http://dx.doi.org/10.1115/1.2928002.

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A methodology is presented for simulating turbomachinery blade rows in a multistage environment by deploying a standard three-dimensional Navier–Stokes solver simultaneously on a number of blade rows. The principal assumptions are that the flow is steady relative to each blade row individually and that the rows can communicate via inter-row mixing planes. These mixing planes introduce circumferential averaging of flow properties but preserve quite general radial variations. Additionally, each blade can be simulated in three-dimensional or axisymmetrically (in the spirit of throughflow analysis

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6

Stelmach, Jacek, Czesław Kuncewicz, Łukasz Adrian, Tomaš Jirout, and Frantisek Rieger. "Change in Mixing Power of a Two-PBT Impeller When Emptying a Tank." Processes 9, no. 2 (2021): 341. http://dx.doi.org/10.3390/pr9020341.

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The paper presents research on the phenomenon of an increase in mixing power during the emptying of a tank with two 6-PBT45° axial impellers in operation, located on a common shaft, pumping the liquid to the bottom of the mixing tank. A large increase in mixing power took place when the free surface of the liquid was just above the upper edge of one of the impellers (hp/D < 0.1). This increase was even more than 50% compared to the design power for a fully filled mixing vessel. Admittedly, high motor overload, while not very long, may damage it. The study investigated the instantaneous torq

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Gevorkyan, L., T. Shoji, D. R. Getsinger, O. I. Smith, and A. R. Karagozian. "Transverse jet mixing characteristics." Journal of Fluid Mechanics 790 (February 2, 2016): 237–74. http://dx.doi.org/10.1017/jfm.2016.5.

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This experimental study explores and quantifies mixing characteristics associated with a gaseous round jet injected perpendicularly into cross-flow for a range of flow and injection conditions. The study utilizes acetone planar laser-induced fluorescence imaging to determine mixing metrics in both centreplane and cross-sectional planes of the jet, for a range of jet-to-cross-flow momentum flux ratios ($2\leqslant J\leqslant 41$), density ratios ($0.35\leqslant S\leqslant 1.0$) and injector configurations (flush nozzle, flush pipe and elevated nozzle), all at a fixed jet Reynolds number of 1900

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8

Hart, M., T. Koga, and Y. Takano. "Mixing Symmetric and Oblique Bragg Reflections in Rigid Channel-Cut Crystals." Journal of Applied Crystallography 28, no. 5 (1995): 568–70. http://dx.doi.org/10.1107/s0021889895003992.

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Because the Bragg angle and Darwin range of total reflection in symmetric and oblique Bragg reflections vary with the angle between the Bragg planes and the crystal surface, it is generally believed that the resulting mismatch causes a loss of intensity in monolithic channel-cut crystals that is unacceptable in practice. It has been discovered that in the unique case of the 220 Bragg reflection from germanium no mismatch occurs, so that oblique and symmetric reflections can be mixed in one rigid channel-cut crystal. The results are valid for both X-ray and neutron channel-cut monochromators.

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Kapulla, R., U. Doll, E. Kirkby, S. Paranjape, and D. Paladino. "Growth laws and self-similarity in the confined mixing zone of unstratified and strongly stably stratified isokinetic mixing-layers past a splitter plate." Physics of Fluids 34, no. 3 (2022): 035129. http://dx.doi.org/10.1063/5.0082950.

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The velocity U and the mixing scalar field Θ of turbulent wake flows developing downstream of a slender splitter plate were studied experimentally for unstratified and strongly stably stratified conditions in a square channel with water as fluid. The experimental program comprises five different Reynolds numbers spanning [Formula: see text]–60 000 for [Formula: see text] (isokinetic conditions) between the two planar, initially separated streams and five relative density stratifications from [Formula: see text] to 10%, since mixing studies for these stratification strengths are rather limited.

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Lu, Tao, Xing Guo Zhu, Ping Wang, and Wei Yyu Zhu. "Numerical Simulation of Flow and Heat Transfer with Large-Eddy Simulation in a Mixing T-Junction." Applied Mechanics and Materials 152-154 (January 2012): 1319–24. http://dx.doi.org/10.4028/www.scientific.net/amm.152-154.1319.

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In the present paper, large-eddy simulation (LES) based on commercial computational fluid dynamics (CFD) software FLUENT for prediction of flow and heat transfer in a mixing T-junction was completed. Mean and root mean square (RMS) temperature and velocity were defined to describe the distributions and fluctuations of temperature and velocity. Numerical results indicate that profiles between symmetrical planes are almost same and the root mean square temperature and velocity close to the center of the main duct in the downstream are larger than those near the main duct wall. The prediction of

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Dissertations / Theses on the topic "Mixing planes"

1

Ward, Duncan Estcourt. "The two-phase plane turbulent mixing layer /." Title page, contents and abstract only, 1986. http://web4.library.adelaide.edu.au/theses/09PH/09phw257.pdf.

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Hug, Stephan Nicholas. "Scalar mixing and coherent structures in simulations of the plane turbulent mixing layer." Thesis, University of Leicester, 2018. http://hdl.handle.net/2381/42162.

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For more than half a century turbulent mixing layers have been the subject of intense experimental and numerical investigation. With the discovery of primary, spanwise aligned and secondary, streamwise oriented vortices the interest in low and high Reynolds number mixing layers has been invigorated. The immense increase of computational capabilities in recent years has lead to an ever growing number of numerical simulations of mixing layers. However, numerical simulations have had great difficulties in reproductions the structure dynamics and entrainment mechanisms observed in the experiments.

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Nygaard, Kris Jacob. "Spanwise-nonuniform excitation of a plane mixing layer." Diss., The University of Arizona, 1991. http://hdl.handle.net/10150/185497.

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The formation and evolution of secondary vortical structures in a plane mixing layer subjected to spanwise-nonuniform excitation has been studied in a closed-return water facility. It is shown that secondary vortices may result from spanwise-nonuniformities in the nominally two-dimensional vorticity layer close to the flow partition, or from spanwise core deformations of the primary vortices further downstream. These distinctly different mechanisms are excited by time-harmonic wavetrains with spanwise amplitude or phase variations, respectively, synthesized by a mosaic of surface film heaters

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Gu, Xiaogang. "Three-dimensional pulsed disturbances in a plane mixing layer." Diss., The University of Arizona, 1994. http://hdl.handle.net/10150/186970.

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The evolution of 3-D pulsed disturbances in a plane mixing layer is studied experimentally. The disturbance is effected via amplitude modulation of a spanwise uniform time-harmonic wave train which provides a clear phase reference for the phase-locked velocity measurements. The evolution of the pulsed disturbance depends critically on the time delay between the modulation pulse and the carrier wave train, the plane mixing layer is most receptive to pulsed excitation when the pulse appears in the braid region between adjacent primary vortices of the base flow. An amplitude demodulation techniqu

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Le, Van Cuong. "Étude sur modèle physique du renforcement des sols par colonnes en « Soil-Mix » : application aux plates-formes ferroviaires." Thesis, Paris Est, 2014. http://www.theses.fr/2014PEST1029/document.

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Ce travail de thèse porte sur l'étude du renforcement par «soil-mixing» des plateformes ferroviaires en France. Cette recherche, à dominante expérimentale, s'appuie sur une approche du type modélisation physique. Deux cas d'études ont été abordés, la dégradation du frottement à l'interface sol-colonne et le comportement mécanique du matériau « soil-mix » à jeune âge sous l'effet de chargements cycliques. En ce qui concerne l'étude du comportement de l'interface entre la colonne en «soil-mix» et le sol environnant, on a développé un essai de chargement d'un tronçon modèle de colonne instrumenté

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YAGAMI, Hisanori, and Tomomi UCHIYAMA. "Numerical Simulation of Particle-Laden Plane Mixing Layer by Three-Dimensional Vortex Method." The Japan Society of Mechanical Engineers, 2006. http://hdl.handle.net/2237/9219.

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Wiltse, John Michael. "Control of mixing in a nonreactive plane shear layer: I. Open-loop control. II. Feedback control." Diss., The University of Arizona, 1993. http://hdl.handle.net/10150/186580.

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A control system for the enhancement and regulation of mixing in a nonreactive plane shear layer has been developed in a two-stream closed-return water facility. Mixing of a passive scalar is estimated using a thermal analog in which the two streams have uniform, steady temperatures differing by 3°C. The position of the temperature interface between the two streams is measured in the plane of its cross stream Schlieren image by an optical sensor which is placed upstream of the rollup of the primary vortices. Control is effected via an array of surface heaters flush-mounted on the flow partitio

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Popish, Martin Roy. "Primary and Secondary Flow Interactions in the Mixing Duct of a 2-D Planer Air Augmented Rocket." DigitalCommons@CalPoly, 2012. https://digitalcommons.calpoly.edu/theses/766.

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Experiments were conducted on the Cal Poly air augmented rocket (AAR) in order to characterize two-dimensional flowfield phenomenon occurring in the mixing duct. The testing utilized a direct connect system where high pressure nitrogen is fed into the combustion chamber, to form a primary flow. The high pressure nitrogen is then expanded through a nozzle, with an area ratio of 22 and an exit area of 0.75 in2, up to Mach 4.3. Secondary air is entrained from a plenum chamber which is used to create a lower stagnation pressure for the secondary flow. The two flows mix in a duct that has a cro

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Chahine, Zakaria. "Contribution a l'etude experimentale de la structure d'une couche de melange plane turbulente developpee." Poitiers, 1987. http://www.theses.fr/1987POIT2280.

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Revue bibliographique. On reprend la decomposition aux valeurs propres de lumley qu'on applique au modele analytique de townsend. Etude experimentale a l'aide de sondes a fil chaud droit et a fil chaud croise. Mesures systematiques des composantes du tenseur des correlations spatiales et spatio-temporelles dans la zone d'affinite. Analyse spectrale des fluctuations de vitesse permettant de distinguer le comportement des trois composantes des fluctuations de vitesse

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Hileman, James Isaac. "Large-scale structures and noise generation in high-speed jets." Connect to this title online, 2004. http://rave.ohiolink.edu/etdc/view?acc%5Fnum=osu1078776079.

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Thesis (Ph. D.)--Ohio State University, 2004.<br>Title from first page of PDF file. Document formatted into pages; contains xxviii, 365 p.; also includes graphics. Includes bibliographical references (p. 269-279).

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Books on the topic "Mixing planes"

1

Ganesh, Raman, and United States. National Aeronautics and Space Administration., eds. Enhanced mixing of a rectangular supersonic jet by natural and induced screech. National Aeronautics and Space Administration, 1993.

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2

K. B. M. Q. Zaman. Streamwise vorticity generation and mixing enhancement in free jets by 'Delta-Tabs'. National Aeronautics and Space Administration, 1993.

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Raman, Ganesh. Mixing and noise benefit versus thrust penalty in supersonic jets using impingement tones. National Aeronautics and Space Administration, 1994.

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Mekkes, Gregory L. Fuel plume image mixing analysis formulation with proper treatment of non-constant velocity flowfields. National Aeronautics and Space Administration, Langley Research Center, 2000.

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5

Bell, James H. Three-dimensional structure of plane mixing layers. Stanford University, Dept. of Aeronautics and Astronautics, 1989.

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6

Moser, R. D. The three-dimensional evolution of a plane mixing layer. National Aeronautics and Space Administration, Ames Research Center, 1992.

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Moser, R. D. The three-dimensional evolution of a plane mixing layer. National Aeronautics and Space Administration, Ames Research Center, 1992.

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Moser, R. D. The three-dimensional evolution of a plane mixing layer. National Aeronautics and Space Administration, Ames Research Center, 1992.

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9

D, Moser R., and Ames Research Center, eds. The three-dimensional evolution of a plane mixing layer. National Aeronautics and Space Administration, Ames Research Center, 1991.

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Moser, Robert D. The three-dimensional evolution of a plane mixing layer. National Aeronautics and Space Administration, Ames Research Center, 1992.

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Book chapters on the topic "Mixing planes"

1

Atreya, Sushil K. "Vertical Mixing." In Atmospheres and Ionospheres of the Outer Planets and Their Satellites. Springer Berlin Heidelberg, 1986. http://dx.doi.org/10.1007/978-3-642-71394-1_4.

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Klingbeil, Knut, Hans Burchard, Sergey Danilov, Claus Goetz, and Armin Iske. "Reducing Spurious Diapycnal Mixing in Ocean Models." In Mathematics of Planet Earth. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-05704-6_8.

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Hetland, Robert D. "Spreading and Mixing in Near-Field River Plumes." In Mathematics of Planet Earth. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-09559-7_8.

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Hartmann, Lee. "Observational Constraints on Transport (And Mixing) in Pre-Main Sequence Disks." In From Dust to Terrestrial Planets. Springer Netherlands, 2000. http://dx.doi.org/10.1007/978-94-011-4146-8_5.

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Fyfe, W. S. "Geosphere Interactions On A Convecting Planet: Mixing and Separation." In The Natural Environment and the Biogeochemical Cycles. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-540-46995-7_1.

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Nygaard, K. J., and A. Glezer. "On the Spanwise Structure of a Plane Mixing Layer." In Advances in Turbulence 2. Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-83822-4_69.

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Lodders, Katharina. "An Oxygen Isotope Mixing Model for the Accretion and Composition of Rocky Planets." In From Dust to Terrestrial Planets. Springer Netherlands, 2000. http://dx.doi.org/10.1007/978-94-011-4146-8_22.

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Dianat, M., Z. Yang, and J. J. McGuirk. "Large-Eddy Simulation of a Two-Phase Plane Mixing-Layer." In Springer Proceedings in Physics. Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-03085-7_187.

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Kaul, Upender K. "On Some Aspects of Wave Interactions in Plane Mixing Layers." In Wave Phenomena. Springer New York, 1989. http://dx.doi.org/10.1007/978-1-4613-8856-2_11.

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Ma, H. D., H. L. Pan, and Q. Wang. "Numerical Simulations of Transitional and Turbulent Flows in Plane Mixing Layers." In Computational Mechanics. Springer Berlin Heidelberg, 2007. http://dx.doi.org/10.1007/978-3-540-75999-7_9.

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Conference papers on the topic "Mixing planes"

1

Zhang, Chenxi, Yang Liu, and Xiao-jing Yu. "Mixing Enhancement Using Secondary Gas Ejection Method in Supersonic-Subsonic Mixing Layer." In 21st AIAA International Space Planes and Hypersonics Technologies Conference. American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-2421.

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RIGGINS, D., C. MCCLINTON, and R. ROGERS. "Flow enthalpy effects on scramjet mixing and combustion." In AlAA 4th International Aerospace Planes Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-5097.

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WOOD, C., and J. SCHETZ. "Effects of unsteady shock impingement on high-speed gaseous mixing." In 3rd International Aerospace Planes Conference. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-5091.

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RAUL, R., H. GILREATH, and G. SULLINS. "Numerical and experimental investigation of mixing enhancement in scramjets." In AlAA 4th International Aerospace Planes Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-5063.

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QUAN, VICTOR, DONALD SMITH, ATUL MATHUR, and RAYMOND EDELMAN. "A three-dimensional approach for analysis of sidewall injector mixing and combustion." In 2nd International Aerospace Planes Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-5243.

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Sekar, Balu. "Conceptual studies of high speed combustors for mixing enhancement mechanisms." In International Aerospace Planes and Hypersonics Technologies. American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-6095.

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Roe, Kevin, Rajeev Thakur, Thong Dang, and Edward Bogucz. "Implementation of a 3D mixing layer code on parallel computers." In International Aerospace Planes and Hypersonics Technologies. American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-6111.

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Gonor, Alexander, Mikhail Gilinsky, Vitali Khaikine, and Isaiah Blankson. "Development of Mixing Analogy for Investigation of Injectant Mixing in Supersonic Flow." In AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-3234.

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Holmes, D. Graham. "Mixing Planes Revisited: A Steady Mixing Plane Approach Designed to Combine High Levels of Conservation and Robustness." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-51296.

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The use of “mixing planes” for steady multistage turbomachinery calculations has been common for some time. The basic idea is simple: in order to perform quasi-steady multistage turbomachinery calculations, the exchange of information at an interface between stationary and rotating blade rows must involve a pitchwise averaging process. This pitchwise averaging implies a mixing process of some sort, which may or may not have a physical analog. This paper revisits the mixing plane idea, and describes an attempt to produce a novel mixing plane algorithm that achieves several key goals, including

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BILLIG, F., and J. SCHETZ. "Analysis of penetration and mixing of gas jets in supersonic cross flow." In AlAA 4th International Aerospace Planes Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-5061.

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Reports on the topic "Mixing planes"

1

Wygnanski, I., and I. Weisbrot. On the Pairing Process in an Excited, Plane, Turbulent Mixing Layer. Defense Technical Information Center, 1987. http://dx.doi.org/10.21236/ada186355.

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Glezer, Ari, and Frank H. Champagne. Real-Time Adaptive Control of Mixing in a Plane Shear Layer. Defense Technical Information Center, 1993. http://dx.doi.org/10.21236/ada285541.

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Aikin, Jr., Robert M. Interim Report on Mixing During the Casting of LEU-10Mo Plates in the Triple Plate Molds. Office of Scientific and Technical Information (OSTI), 2017. http://dx.doi.org/10.2172/1352396.

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Loucks, Richard B. An Experimental Examination of the Streamwise Velocity in a Plane Mixing Layer using a Single Hot-Wire Sensor. Defense Technical Information Center, 1997. http://dx.doi.org/10.21236/ada332948.

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Mikkelsen, D. R. Solution of the Fokker-Planck equation with mixing of angular harmonics by beam-beam charge exchange. Office of Scientific and Technical Information (OSTI), 1989. http://dx.doi.org/10.2172/5577657.

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Miller, Timothy C. Mode Mixity Determinations for Interfacial Cracking in Incompressible Materials Under Plane Strain Conditions. Defense Technical Information Center, 1998. http://dx.doi.org/10.21236/ada409481.

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Onishi, Y., and J. D. Hudson. Waste mixing and diluent selection for the planned retrieval of Hanford Tank 241-SY-102: A preliminary assessment. Office of Scientific and Technical Information (OSTI), 1996. http://dx.doi.org/10.2172/176772.

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Manor, M. J., and S. J. Piercey. Whole-rock lithogeochemistry, Nd-Hf isotopes, and in situ zircon geochemistry of VMS-related felsic rocks, Finlayson Lake VMS district, Yukon. Natural Resources Canada/CMSS/Information Management, 2021. http://dx.doi.org/10.4095/328992.

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The Finlayson Lake district in southeastern Yukon is composed of a Late Paleozoic arc-backarc system that consists of metamorphosed volcanic, plutonic, and sedimentary rocks of the Yukon-Tanana and Slide Mountain terranes. These rocks host &amp;gt;40 Mt of polymetallic resources in numerous occurrences and styles of volcanogenic massive sulphide (VMS) mineralization. Geochemical and isotopic data from these rocks support previous interpretations that volcanism and plutonism occurred in arc-marginal arc (e.g., Fire Lake formation) and continental back-arc basin environments (e.g., Kudz Ze K

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Pearlstein, Arne J. Global Two-Scalar Velocimetry and Development of Low-Order Models for Use in Optical-Phase Correction in a Plane Mixing Layer. Defense Technical Information Center, 2000. http://dx.doi.org/10.21236/ada376026.

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Seginer, Ido, Daniel H. Willits, Michael Raviv, and Mary M. Peet. Transpirational Cooling of Greenhouse Crops. United States Department of Agriculture, 2000. http://dx.doi.org/10.32747/2000.7573072.bard.

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Abstract:

Background Transplanting vegetable seedlings to final spacing in the greenhouse is common practice. At the time of transplanting, the transpiring leaf area is a small fraction of the ground area and its cooling effect is rather limited. A preliminary modeling study suggested that if water supply from root to canopy is not limiting, a sparse crop could maintain about the same canopy temperature as a mature crop, at the expense of a considerably higher transpiration flux per leaf (and root) area. The objectives of this project were (1) to test the predictions of the model, (2) to select suitable

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