Relevant bibliographies by topics / Moderate reynolds

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

Academic literature on the topic 'Moderate reynolds'

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

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Journal articles on the topic "Moderate reynolds"

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Tam, Christopher K. W., and Hongbin Ju. "Aerofoil tones at moderate Reynolds number." Journal of Fluid Mechanics 690 (December 1, 2011): 536–70. http://dx.doi.org/10.1017/jfm.2011.465.

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AbstractIt is known experimentally that an aerofoil immersed in a uniform stream at a moderate Reynolds number emits tones. However, there have been major differences in the experimental observations in the past. Some experiments reported the observation of multiple tones, with strong evidence that these tones are most probably generated by a feedback loop. There is also an experiment reporting the observation of a single tone with no tonal jump or other features associated with feedback. In spite of the obvious differences in the experimental observations published in the literature, it is noted that all the dominant tone frequencies measured in all the investigations are in agreement with an empirically derived Paterson formula. The objective of the present study is to perform a direct numerical simulation (DNS) of the flow and acoustic phenomenon to investigate the tone generation mechanism. When comparing with experimental studies, numerical simulations appear to have two important advantages. The first is that there is no background wind tunnel noise in numerical simulation. This avoids the signal-to-noise ratio problem inherent in wind tunnel experiments. In other words, it is possible to study tones emitted by a truly isolated aerofoil computationally. The second advantage is that DNS produces a full set of space–time data, which can be very useful in determining the tone generation processes. The present effort concentrates on the tones emitted by three NACA0012 aerofoils with a slightly rounded trailing edge but with different trailing edge thickness at zero degree angle of attack. At zero degree angle of attack, in the Reynolds number range of$2\ensuremath{\times} 1{0}^{5} $to$5\ensuremath{\times} 1{0}^{5} $, the boundary layer flow is attached nearly all the way to the trailing edge of the aerofoil. Unlike an aerofoil at an angle of attack, there is no separation bubble, no open flow separation. All the flow separation features tend to increase the complexity of the tone generation processes. The present goal is limited to finding the basic tone generation mechanism in the simplest flow configuration. Our DNS results show that, for the flow configuration under study, the aerofoil emits only a single tone. This is true for all three aerofoils over the entire Reynolds number range of the present study. In the literature, it is known that Kelvin–Helmholtz instabilities of free shear layers generally have a much higher spatial growth rate than that of the Tollmien–Schlichting boundary layer instabilities. A near-wake non-parallel flow instability analysis is performed. It is found that the tone frequencies are the same as the most amplified Kelvin–Helmholtz instability at the location where the wake has a minimum half-width. This suggests that near-wake instability is the energy source of aerofoil tones. However, flow instabilities at low subsonic Mach numbers generally do not cause strong tones. An investigation of how near-wake instability generates tones is carried out using the space–time data provided by numerical simulations. Our observations indicate that the dominant tone generation process is the interaction of the oscillatory motion of the near wake, driven by flow instability, with the trailing edge of the aerofoil. Secondary mechanisms involving unsteady near-wake motion and the formation of discrete vortices in regions further downstream are also observed.
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Bershadskii, A. G. "Turbulence singularities at moderate reynolds numbers." Journal of Engineering Physics 58, no. 6 (June 1990): 703–6. http://dx.doi.org/10.1007/bf00872720.

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KNAEPEN, B., S. KASSINOS, and D. CARATI. "Magnetohydrodynamic turbulence at moderate magnetic Reynolds number." Journal of Fluid Mechanics 513 (August 25, 2004): 199–220. http://dx.doi.org/10.1017/s0022112004000023.

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L’vov, Victor S., and Itamar Procaccia. "Extended universality in moderate-Reynolds-number flows." Physical Review E 49, no. 5 (May 1, 1994): 4044–51. http://dx.doi.org/10.1103/physreve.49.4044.

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Ruschak, Kenneth J., and Steven J. Weinstein. "Thin-Film Flow at Moderate Reynolds Number." Journal of Fluids Engineering 122, no. 4 (July 5, 2000): 774–78. http://dx.doi.org/10.1115/1.1319499.

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Viscous, laminar, gravitationally-driven flow of a thin film over a round-crested weir is analyzed for moderate Reynolds numbers. A previous analysis of this flow utilized a momentum integral approach with a semiparabolic velocity profile to obtain an equation for the film thickness (Ruschak, K. J., and Weinstein, S. J., 1999, “Viscous Thin-Film Flow Over a Round-Crested Weir,” ASME J. Fluids Eng., 121, pp. 673–677). In this work, a viscous boundary layer is introduced in the manner of Haugen (Haugen, R., 1968, “Laminar Flow Around a Vertical Wall,” ASME J. Appl. Mech. 35, pp. 631–633). As in the previous analysis of Ruschak and Weinstein, the approximate equations have a critical point that provides an internal boundary condition for a bounded solution. The complication of a boundary layer is found to have little effect on the thickness profile while introducing a weak singularity at its beginning. The thickness of the boundary layer grows rapidly, and there is little cumulative effect of the increased wall friction. Regardless of whether a boundary layer is incorporated, the approximate free-surface profiles are close to profiles from finite-element solutions of the Navier-Stokes equation. Similar results are obtained for the related problem of developing flow on a vertical wall (Cerro, R. L., and Whitaker, S., 1971, “Entrance Region Flows With a Free Surface: the Falling Liquid Film,” Chem. Eng. Sci., 26, pp. 785–798). Less accurate results are obtained for decelerating flow on a horizontal wall (Watson, E. J., 1964, “The Radial Spread of a Liquid Jet Over a Horizontal Plane,” J. Fluid Mech. 20, pp. 481–499) where the flow is not gravitationally driven. [S0098-2202(00)01904-0]
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Zamyshlyaev, A. A., and G. R. Shrager. "Fluid Flows past Spheroids at Moderate Reynolds Numbers." Fluid Dynamics 39, no. 3 (May 2004): 376–83. http://dx.doi.org/10.1023/b:flui.0000038556.08179.ea.

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Kotas, C. W., M. Yoda, and P. H. Rogers. "Visualizations of steady streaming at moderate Reynolds numbers." Physics of Fluids 18, no. 9 (September 2006): 091102. http://dx.doi.org/10.1063/1.2335902.

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Bandaru, Vinodh, Thomas Boeck, and Jörg Schumacher. "Hartmann duct flow at moderate magnetic Reynolds numbers." PAMM 16, no. 1 (October 2016): 577–78. http://dx.doi.org/10.1002/pamm.201610277.

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Smith, T. A., and Y. Ventikos. "Wing-tip vortex dynamics at moderate Reynolds numbers." Physics of Fluids 33, no. 3 (March 1, 2021): 035111. http://dx.doi.org/10.1063/5.0039492.

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HILL, REGHAN J., and DONALD L. KOCH. "Moderate-Reynolds-number flow in a wall-bounded porous medium." Journal of Fluid Mechanics 453 (February 25, 2002): 315–44. http://dx.doi.org/10.1017/s002211200100684x.

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The transition to unsteady flow and the dynamics of moderate-Reynolds-number flows in unbounded and wall-bounded periodic arrays of aligned cylinders are examined using lattice-Boltzmann simulations. The simulations are compared to experiments, which necessarily have bounding walls. With bounding walls, the transition to unsteady flow is accompanied by a loss of spatial periodicity, and the temporal fluctuations are chaotic at much smaller Reynolds numbers. The walls, therefore, affect the unsteady flows everywhere in the domain. Consistency between experiments and simulations is established by examining the wake lengths for steady flows and the fundamental frequencies at higher Reynolds numbers, both as a function of the Reynolds number. Simulations are used to examine the velocity fluctuations, flow topologies, and the fluctuating forces on the cylinders.
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Dissertations / Theses on the topic "Moderate reynolds"

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Biswas, Anupam. "Hydrodynamic interaction between cylinders at moderate Reynolds numbers." Thesis, University of British Columbia, 2013. http://hdl.handle.net/2429/44730.

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The hydrodynamic interaction between two cylinders perpendicular to the freestream, in a tandem arrangement was studied for moderate Reynolds numbers (1≤Re≤40). The influence of multiple geometric variables was considered: separation distances between the cylinders, ellipticity of the cylinders, the cylinder aspect ratio, and the angular inclination between the cylinders. In the first part of this study, a numerical investigation of the two-dimensional steady flow past cylinders was carried out. The characteristic length, D, in all simulations was taken to be twice the major axis of the cylinder cross-section, (i.e. equal to the diameter for cylinders of circular cross-section). The two-dimensional flow was studied for separations up to 50D. Four different ellipticities were studied. The drags experienced by front and rear cylinders were compared with that experienced by a single cylinder of the same cross-section. The second part of the study consisted of the steady three-dimensional flow analysis for parallel cylinders in tandem for separations ranging from 2D to 20D and cylinder lengths up to 20D. In the third part of this thesis, a steady flow analysis was done for two circular cylinders in tandem with lengths equal to 5D but with the cylinder axes in different orientations relative to the plane normal to the flow. This angular separation between the cylinders produces a hydrodynamic moment, which is dependent on the geometry and the flow Reynolds number. The fourth and final part of this work is the study of the unsteady three-dimensional flow that would result from the hydrodynamic moment discussed in relation to the third part of the thesis. The thesis closes with some remarks on the implications of these findings to papermaking and recommendations for future work.
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Tang, Tongdar Danny. "Periodic flow in a bifurcating tube at moderate reynolds number." Diss., Georgia Institute of Technology, 1990. http://hdl.handle.net/1853/17066.

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Sirisup, Sirod. "Linear stability of plane Couette flow at moderate Reynolds numbers." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk3/ftp04/mq64453.pdf.

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Van, Hirtum Annemie. "Moderate Reynolds number flow. Application to the human upper airways." Habilitation à diriger des recherches, Université de Grenoble, 2011. http://tel.archives-ouvertes.fr/tel-00747213.

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The study of fluid flow is an amasingly ordinary as well as fascinating subject. During the past few years I had the opportunity to work as a researcher in the field of fluid flow modelling applied to airflow through the human upper airways and related phenomena such as speech production, . . . The current document is a brief report on the research to which I participated aiming a small contribution to this rich and stimulating research area.
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Giacobello, Matteo. "Wake structure of a transversely rotating sphere at moderate Reynolds numbers." Online version, 2005. http://repository.unimelb.edu.au/10187/2840.

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Over the last century, the problem of a viscous flow past a sphere has received on-going attention due to its many engineering applications. These include combustion processes, sediment transport processes and atmospheric flow problems, where the sphere serves as a good model for more general bluff body particles. In these environments, particles may be subjected to both translational and rotational velocities. The objective of this study was to investigate the effect that sphere rotation, about an axis transverse to the freestream flow, has on the characteristics or the vertical wake structure and the forces exerted on the sphere. That was achieved by solving the time-dependant, incompressible Navier Stokes equations, using a highly accurate Fourier Chebyshev spectral collation method.
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Bell, Martin Derek. "Ordering of particulate suspensions in Couette flow at moderate Reynolds numbers." Thesis, University of British Columbia, 1990. http://hdl.handle.net/2429/28901.

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A remarkable ordering phenomenon has been seen to occur when a suspension of particles undergoes shear at particle Reynolds numbers of the order of or greater than one in the annular gap of a Couette type shearing device. This particulate ordering was observed and studied with both suspensions of rigid spheres and suspensions of polystyrene latex aggregates formed in the presence of shear within the gap. Each of these systems was studied under a variety of initial conditions in order to define the particular flow conditions required for particle alignment to occur. It was found that particulate ordering occurred under similar conditions to those used by Segré and Silberberg (35) to observe the "necklace formations" that formed within particulate suspensions flowing inside tubes. The separations between aligned particles was found to be strongly dependent on the particle Reynolds number and the ratio between the particle diameter and the width of the annular gap. An insight into the hydrodynamic interactions occurring was provided by the comparisons made between the ordered aggregates and the ordered rigid spheres under similar flow conditions.
Science, Faculty of
Chemistry, Department of
Graduate
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Konozsy, Laszlo. "Multiphysics CFD modelling of incompressible flows at Low and Moderate Reynolds Numbers." Thesis, Cranfield University, 2012. http://dspace.lib.cranfield.ac.uk/handle/1826/7860.

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In this Ph.D. thesis, a novel high-resolution Godunov-type numerical procedure has been developed for solving the unsteady, incompressible Navier-Stokes equations for constant and variable density flows. The proposed FSAC-PP approach encompasses both artificial compressibility (AC) and fractional step (FS) pressure-projection (PP) methods of Chorin [3, 4] in a unified solution concept. To take advantage of different computational strategies, the FS and AC methods have been coupled (FSAC formulation), and further a PP step has been employed at each pseudo-time step. To provide time-accurate solutions, the dual-time stepping procedure is utilized. Taking the advantage of the hyperbolic nature of the inviscid part of the AC formulation, high-resolution characteristics-based (CB) Godunov-type scheme is employed to discretize the non-linear advective fluxes. Highorder of accuracy is achieved by using from first- up to ninth-order interpolation schemes. Time integration is obtained from a fourth-order Runge-Kutta scheme. A non-linear fullmultigrid, full-approximation storage (FMG-FAS) acceleration technique has been further extended to the FSAC-PP solution method to increase the efficiency and decrease the computational cost of the developed method and simulations. Cont/d.
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Beirutty, Mohammad Hussein. "Development of a hot-wire measurement technique for moderate intensity three-dimensional flows /." Thesis, Connect to this title online; UW restricted, 1987. http://hdl.handle.net/1773/7074.

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Oshida, Takeshi. "Surface equation of falling film flows with moderate Reynolds number and large but finite Weber number." 京都大学 (Kyoto University), 2000. http://hdl.handle.net/2433/181170.

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Patrick, Wilfred Vinod. "Computations of Flow Structures and Heat Transfer in a Dimpled Channel at Low to Moderate Reynolds Number." Thesis, Virginia Tech, 2005. http://hdl.handle.net/10919/33415.

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Time-accurate calculations are used to investigate the three-dimensional flow structure and understand its influence on the heat transfer in a channel with concave indentations on one wall. A dimple depth to channel height ratio of 0.4 and dimple depth to imprint diameter ratio of 0.2 is used in the calculations. The Reynolds number (based on channel height) varies from Re = 25 in the laminar regime to Re = 2000 in the early turbulent regime. Fully developed flow and heat transfer conditions were assumed and a constant heat flux boundary condition was applied to the walls of the channel. In the laminar regime, the flow and heat transfer characteristics are dominated by the recirculation zones in the dimple with resulting augmentation ratios below unity. Flow transition is found to occur between Re = 1020 and 1130 after which both heat transfer and friction augmentation increase to values of 3.22 and 2.75, respectively, at Re = 2000. The presence of large scale vortical structures ejected from the dimple cavity dominate all aspects of the flow and heat transfer, not only on the dimpled surface but also on the smooth wall. In all cases the thermal efficiency using dimples was found to be significantly larger than other heat transfer augmentation techniques currently employed.
Master of Science
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Books on the topic "Moderate reynolds"

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Succi, Sauro. Flows at Moderate Reynolds Numbers. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199592357.003.0018.

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This chapter presents the application of LBE to flows at moderate Reynolds numbers, typically hundreds to thousands. This is an important area of theoretical and applied fluid mechanics, one that relates, for instance, to the onset of nonlinear instabilities and their effects on the transport properties of the unsteady flow configuration. The regime of Reynolds numbers at which these instabilities take place is usually not very high, of the order of thousands, hence basically within reach of present day computer capabilities. Nonetheless, following the full evolution of these transitional flows requires very long-time integrations with short time-steps, which command substantial computational power. Therefore, efficient numerical methods are in great demand. Also of major interest are steady-state or pulsatile flows at moderate Reynolds numbers in complex geometries, such as they occur, for instance, in hemodynamic applications. The application of LBE to such flows will also briefly be mentioned
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Book chapters on the topic "Moderate reynolds"

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Kalliadasis, S., C. Ruyer-Quil, B. Scheid, and M. G. Velarde. "Modeling Methodologies for Moderate Reynolds Number Flows." In Applied Mathematical Sciences, 145–92. London: Springer London, 2012. http://dx.doi.org/10.1007/978-1-84882-367-9_6.

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Langbein, D. "Drop and Bubble Migration at Moderate Reynolds and Marangoni Numbers." In Microgravity Fluid Mechanics, 413–25. Berlin, Heidelberg: Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-50091-6_43.

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Zapryanov, Z., and S. Tabakova. "Finite Deformations of Drops and Bubbles at Moderate Reynolds Numbers Flows." In Dynamics of Bubbles, Drops and Rigid Particles, 437–86. Dordrecht: Springer Netherlands, 1999. http://dx.doi.org/10.1007/978-94-015-9255-0_14.

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Likhachev, Oleg A. "Coherent Vortical Structures in Plane Far Wakes at Moderate Reynolds Numbers." In Nonlinear Instability of Nonparallel Flows, 340–49. Berlin, Heidelberg: Springer Berlin Heidelberg, 1994. http://dx.doi.org/10.1007/978-3-642-85084-4_29.

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Halim Atallah, Georges, Emmanuel Belut, Sullivan Lechêne, Benoît Trouette, and Stéphane Vincent. "Simulation of a Confined Turbulent Round Jet at Moderate Reynolds Number." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 110–16. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-65820-5_10.

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Iwamoto, Kaoru, Yuji Suzuki, and Nobuhide Kasagi. "Nonlinear Interaction of Coherent Structures in Wall Turbulence at Low-to-Moderate Reynolds Numbers." In IUTAM Symposium on Reynolds Number Scaling in Turbulent Flow, 23–28. Dordrecht: Springer Netherlands, 2004. http://dx.doi.org/10.1007/978-94-007-0997-3_5.

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Hemmati, Arman, David H. Wood, and Robert J. Martinuzzi. "Wake Dynamics Behind a Normal Thin Flat Plate at Moderate Reynolds Numbers." In Springer Proceedings in Physics, 265–69. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-29130-7_46.

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Sirisup, Sirod, and Saifhon Tomkratoke. "Proper Orthogonal Decomposition of Unsteady Heat Transfer from Staggered Cylinders at Moderate Reynolds Numbers." In Computational Fluid Dynamics 2008, 763–69. Berlin, Heidelberg: Springer Berlin Heidelberg, 2009. http://dx.doi.org/10.1007/978-3-642-01273-0_101.

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Bolemann, T., A. Beck, D. Flad, H. Frank, V. Mayer, and C. D. Munz. "High-Order Discontinuous Galerkin Schemes for Large-Eddy Simulations of Moderate Reynolds Number Flows." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 435–56. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-12886-3_20.

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Prokudina, L., and Ye Salamatov. "Simulation of Counter-Current Gas Flow in Falling-Film Equipment for Moderate Reynolds Numbers." In Lecture Notes in Mechanical Engineering, 1026–35. Cham: Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-54814-8_118.

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Conference papers on the topic "Moderate reynolds"

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Gai, S. L., R. Prakash, A. Khraibut, L. Le Page, and S. O’Byrne. "Large scale hypersonic separated flows at moderate Reynolds numbers and moderate density." In 31ST INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS: RGD31. AIP Publishing, 2019. http://dx.doi.org/10.1063/1.5119600.

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Bernero, Stefano, and Sastry Munukutla. "Turbulent pipe flow development at moderate Reynolds numbers." In Fluid Dynamics Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1995. http://dx.doi.org/10.2514/6.1995-2247.

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Yakovenko, Sergey N. "Modeling of plane jet at moderate Reynolds numbers." In PROCEEDINGS OF THE XXV CONFERENCE ON HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2017): Dedicated to the 60th anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. Author(s), 2017. http://dx.doi.org/10.1063/1.5007559.

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Thomas, Susan, and Tim Ameel. "Moderate Reynolds Number Mixing in a T-Channel." In ASME 2010 8th International Conference on Nanochannels, Microchannels, and Minichannels collocated with 3rd Joint US-European Fluids Engineering Summer Meeting. ASMEDC, 2010. http://dx.doi.org/10.1115/fedsm-icnmm2010-30159.

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An experimental investigation of water flow in a T-shaped channel with rectangular cross section (20 × 20 mm inlet ID and 20 × 40 mm outlet ID) has been conducted for a Reynolds number Re range of 56 to 422, based on inlet diameter. Dynamical conditions and the T-channel geometry of the current study are applicable to the microscale. This study supports a large body of numerical work, and resolution and the interrogation region are extended beyond previous experimental studies. Laser induced fluorescence (LIF) and particle imaging velocimetry (PIV) are used to characterize flow behaviors over the broad range of Re where realistic T-channels operate. Scalar structures previously unresolved in the literature are presented. Special attention is paid to the unsteady flow regimes that develop at moderate Re, which significantly impact mixing but are not yet well characterized or understood. An unsteady symmetric topology, which develops at higher Re and negatively impacts mixing, is presented, and mechanisms behind the wide range of mixing qualities predicted for this regime are explained. An optimal Re operating range is identified based on multiple experimental trials.
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GHONIEM, A., and Y. GAGNON. "Numerical investigations of recirculating flow at moderate Reynolds numbers." In 24th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-370.

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Tam, Christopher, and Hongbin Ju. "Airfoil Tones at Moderate Reynolds Number: A Computational Study." In 17th AIAA/CEAS Aeroacoustics Conference (32nd AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-2711.

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Gallis, M. A., J. R. Torczynski, N. P. Bitter, T. P. Koehler, S. G. Moore, S. J. Plimpton, and G. Papadakis. "DSMC simulations of turbulent flows at moderate Reynolds numbers." In 31ST INTERNATIONAL SYMPOSIUM ON RAREFIED GAS DYNAMICS: RGD31. AIP Publishing, 2019. http://dx.doi.org/10.1063/1.5119564.

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MACE, J., and T. ADAMSON, JR. "Shock waves in transonic channel flows at moderate Reynolds number." In 23rd Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1985. http://dx.doi.org/10.2514/6.1985-369.

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Li, Guojun, Boo Cheong Khoo, and Rajeev K. Jaiman. "Computational aeroelasticity of flexible membrane wings at moderate Reynolds numbers." In AIAA Scitech 2020 Forum. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2020. http://dx.doi.org/10.2514/6.2020-2036.

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Mascarenhas, Brendan, and Brian Helenbrook. "Wind Turbine Wake Behavior at Moderate Reynolds Numbers as Predicted by Reynolds-Averaged-Navier-Stokes Models." In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-1103.

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