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Artykuły w czasopismach na temat "Reynolds's number"

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Sandulyak, Anna, Alexander Sandulyak, Maria Polismakova, Darya Sandulyak, and Vera Ershova. "About Transition Reynolds Number of Filtration Magnetophoresis Process." Applied Mechanics and Materials 851 (August 2016): 127–31. http://dx.doi.org/10.4028/www.scientific.net/amm.851.127.

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In this present work, the approaches providing establishment of transitional value of Reynolds number when filtering liquids in the magnetized granulated (polyspherical) matrix are considered. It is shown that value of transitional number of Reynolds by flow through the granulated matrix is not crisis for process of a magnetophoresis. It is confirmed on the example of magnetophoresis of ferroparticles in water suspension, thermal power plant condensate, liquid ammonia. It is established that the effective of magnetophoresis could be performed also in case of Reynolds's values much more than de
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Górecki, Piotr. "A View from a Distance." Law and History Review 21, no. 2 (2003): 367–76. http://dx.doi.org/10.2307/3595096.

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Susan Reynolds's article is a culmination and a turning point. It builds on several approaches to medieval law and culture, of which two strike me as especially important. One is a study of legal history as a domain of human activity, especially habitual or routine activity, pursued by a wide range of social groups. The other is a search for the meaning and the criteria of the enormous transition during the central Middle Ages, which Christopher Dawson at the dawn of this subject, and Robert Bartlett in its currently definitive moment, have identified as “the making of Europe.” The first subje
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Hoang, Duc N. M., Duc M. Tran, Thanh-Sang Tran, and Hoang-Anh Pham. "An adaptive weighting mechanism for Reynolds rules-based flocking control scheme." PeerJ Computer Science 7 (February 16, 2021): e388. http://dx.doi.org/10.7717/peerj-cs.388.

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Cooperative navigation for fleets of robots conventionally adopts algorithms based on Reynolds's flocking rules, which usually use a weighted sum of vectors for calculating the velocity from behavioral velocity vectors with corresponding fixed weights. Although optimal values of the weighting coefficients giving good performance can be found through many experiments for each particular scenario, the overall performance could not be guaranteed due to unexpected conditions not covered in experiments. This paper proposes a novel control scheme for a swarm of Unmanned Aerial Vehicles (UAVs) that a
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Nimish, Dubey Mr. Morrish Kumar. "DESIGN MODIFICATION IN HEAT EXCHANGER TWISTED TAPE FOR HEAT TRANSFER ENHANCEMENT- A REVIEW." INTERNATIONAL JOURNAL OF ENGINEERING SCIENCES & RESEARCH TECHNOLOGY 6, no. 7 (2017): 1–5. https://doi.org/10.5281/zenodo.822920.

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Heat exchangers are very much essential industrial as well as domestic equipment used every day. Overall performance of any machine and many systems as a whole depends on the performance of a heat exchanger. To improve the performance of a heat exchanger it is needed to improve the heat transfer phenomena of a tube. Number of researches has been done to develop devices or means to enhance the performance of a heat exchanger. The most successful development of a component for the most efficient enhancement of heat exchanger performance is development of twisted tape inserts for heat exchanger t
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Kalpana, Soni*1 &. Surendra Bharti2. "CFD ANALYSIS OF SOLAR AIR HEATER FOR ENHANCEMENT OF HEAT TRANSFER." INTERNATIONAL JOURNAL OF ENGINEERING SCIENCES & RESEARCH TECHNOLOGY 6, no. 6 (2017): 430–44. https://doi.org/10.5281/zenodo.814587.

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Energy is the basic ingredient to sustain life and development. Work means moving or lifting something, warming or lighting something. There are many sources of energy that help to run the various machines invented by man.A 3-dimensional CFD analysis has been carried out to study heat transfer and fluid flow behavior in a rectangular duct of a solar air heater with one roughened wall having combination of circularand square transverse wire rib roughness. The effect of Reynolds number, roughness height, roughness pitch, relative roughness pitch and relative roughness height on the heat transfer
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Ajay, Jain, and H. S. Sahu Prof. "CFD Analysis of Solar Air Heater for Enhancenment of Heat Transfer Through Inclined Rib Roughness." International Journal of Trend in Scientific Research and Development 3, no. 1 (2018): 662–67. https://doi.org/10.31142/ijtsrd19057.

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A 3 dimensional CFD analysis has been carried out of solar air heater to study heat transfer and fluid flow behavior in a rectangular duct of a solar air heater with one roughened wall having combination of circular and square transverse wire rib roughness. The effect of Reynolds number, roughness height, roughness pitch, relative roughness pitch and relative roughness height on the heat transfer coefficient and friction factor have been studied. In order to validate the present numerical model, results have been compared with available experimental results under similar flow conditions. CFD I
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Harish, Tiwari, V. Bute Jayesh, and Patil Rupali. "Effects of Non-Dimensional Parameters on the Performance of Three Pass Helical Coil Heat Exchanger." Journal of Industrial Mechanics 4, no. 3 (2019): 1–7. https://doi.org/10.5281/zenodo.3534707.

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Heat exchanger is that device which is used to transfer thermal energy in more than two fluids, between a solid surface and a fluid, at different related temperatures. Heat exchangers are used in various applications and the deserving heat exchangers have major demand from industries. Due to the increasing trend of global industrialization, crucial efforts have been taken to increase the heat transfer, rate of heat transfer, minimize dimensions of heat exchangers, and also increase in the overall effectiveness. The secondary flow develops to the curvature of the tube. The curvature of the coil
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Ajay, Jain, and S. Sahu H. "CFD Analysis of Solar Air Heater Provided with Discrete Inclined Rib Roughness on the Absorber Plate A Review." International Journal of Trend in Scientific Research and Development 2, no. 6 (2018): 703–6. https://doi.org/10.31142/ijtsrd18686.

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Heat transfer enhancement is a subject of considerable interest to researchers as it leads to saving in energy and cost. Because of the rapid increase in energy demand in all over The world, both reducing energy lost related with ineffective use and enhancement of energy in the meaning of heat have become an increasingly significance task for design and operation engineers for many system. A 3 dimensional CFD analysis has been carried out to study heat transfer and fluid flow behavior in a rectangular duct of a solar air heater with one roughened wall having discrete inclined rib roughness. Th
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Wang, S., Y. Zhou, Md Mahbub Alam, and H. Yang. "Turbulent intensity and Reynolds number effects on an airfoil at low Reynolds numbers." Physics of Fluids 26, no. 11 (2014): 115107. http://dx.doi.org/10.1063/1.4901969.

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Vadim, Lemanov, Terekhov Viktor, Sharov Konstantin, and Shumeiko Andrey. "1038 TRANSITIONAL REYNOLDS NUMBER IN SUBMERGED MACRO- AND MICROJETS." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1038–1_—_1038–4_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1038-1_.

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Rozprawy doktorskie na temat "Reynolds's number"

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Tam, Daniel See Wai 1980. "Motion at low Reynolds number." Thesis, Massachusetts Institute of Technology, 2008. http://hdl.handle.net/1721.1/49682.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2008.<br>Includes bibliographical references (p. 181-192).<br>The work described in this thesis centers on inertialess motion at low Reynolds numbers at the crossroad between biofluids and microfluids. Here we address questions regarding locomotion of micro-swimmers, transport of nutrient around micro-organisms as well as mixing and heat exchange inside micro-droplets of water. A general framework for the investigation of optimal locomotion strategies for slender swimmers has been developed and appli
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Slim, Anja Catharina. "High Reynolds number gravity currents." Thesis, University of Cambridge, 2006. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.614096.

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Srinivasa, Murthy P. "Low Reynolds Number Airfoil Aerodynamics." Thesis, Indian Institute of Science, 2000. https://etd.iisc.ac.in/handle/2005/229.

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In this thesis we describe the development of Reynolds- averaged Navier Stokes code for the flow past two- dimensional configuration. Particularly, emphasis has been laid on the study of low Reynolds number airfoil aerodynamics. The thesis consists of five chapters covering the back ground history, problem formulation, method of solution and discussion of the results and conclusion. Chapter I deals with a detailed background history of low Reynolds number aerodynamics, problem associated with it, state of the art, its importance in practical applications in aircraft industries. Chapte
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Srinivasa, Murthy P. "Low Reynolds Number Airfoil Aerodynamics." Thesis, Indian Institute of Science, 2000. http://hdl.handle.net/2005/229.

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In this thesis we describe the development of Reynolds- averaged Navier Stokes code for the flow past two- dimensional configuration. Particularly, emphasis has been laid on the study of low Reynolds number airfoil aerodynamics. The thesis consists of five chapters covering the back ground history, problem formulation, method of solution and discussion of the results and conclusion. Chapter I deals with a detailed background history of low Reynolds number aerodynamics, problem associated with it, state of the art, its importance in practical applications in aircraft industries. Chapter II d
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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 struc
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Wales, Christopher John Alasdair. "Continuation methods for high Reynoldss number compressible flows." Thesis, University of Bristol, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.529897.

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Chebbi, Brahim. "Experiments in low Reynolds number flows." Thesis, University of Ottawa (Canada), 1989. http://hdl.handle.net/10393/5989.

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Erm, Lincoln. "Low-Reynolds-number turbulent boundary layers /." Connect to thesis, 1988. http://eprints.unimelb.edu.au/archive/00000226.

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Stevens, Patrick Robert Robbie James. "Unsteady low Reynolds number aerodynamic forces." Thesis, University of Cambridge, 2015. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.709135.

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Banks, Curtis Alwyn. "Instabilities in high Reynolds number flows." Thesis, Imperial College London, 2015. http://hdl.handle.net/10044/1/29416.

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An asymptotic method for predicting stability characteristics, both stationary and travelling crossflow vortices, over a variety of surface variations was created. These include flat, convex and concave curved surfaces. Comparisons were made with two different numerical methods (Parabolised Stability Equations and Velocity-Vorticity) and good agreement, to within 5% of the numerical value of the crossflow mode streamwise growth rate was met for both stationary and travelling modes initially for a flat surface. An additional comparison was made with the streamwise growth rates to observe the im
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Książki na temat "Reynolds's number"

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J, Yoo G., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. On the modeling of low-Reynolds-number turbulence. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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J, Yoo G., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. On the modeling of low-Reynolds-number turbulence. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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So, Ronald M. C. On the modeling of low-Reynolds-number turbulence. Lewis Research Center, 1986.

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Center, Langley Research, ed. Unstructured and adaptive mesh generation for high Reynolds number viscous flows. National Aeronautics and Space Administration, Langley Research Center, 1991.

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Joseph, Katz. Final report for the grant integration of viscous effects into inviscid computational methods. National Aeronautics and Space Administration, 1990.

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Sandborn, Virgil A. Evaluation of high reynolds number flow in a 180 degree turn-around duct. National Aeronautics and Space Administration, 1991.

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Joseph, Katz. Final report for the grant integration of viscous effects into inviscid computational methods. National Aeronautics and Space Administration, 1990.

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United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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Mueller, Thomas J., ed. Low Reynolds Number Aerodynamics. Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-84010-4.

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Mueller, Thomas J. Low Reynolds number vehicles. Agard, 1985.

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Części książek na temat "Reynolds's number"

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Khonsari, M. M. "Reynolds Number." In Encyclopedia of Tribology. Springer US, 2013. http://dx.doi.org/10.1007/978-0-387-92897-5_147.

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Gooch, Jan W. "Reynolds Number." In Encyclopedic Dictionary of Polymers. Springer New York, 2011. http://dx.doi.org/10.1007/978-1-4419-6247-8_10015.

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Kurzke, Joachim, and Ian Halliwell. "Reynolds Number Corrections." In Propulsion and Power. Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-75979-1_17.

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Kurzke, Joachim, Ian Halliwell, and Robert Hill. "Reynolds Number Corrections." In Propulsion and Power. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-65026-0_23.

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Herwig, Heinz. "Reynolds-Zahl Re (Reynolds number Re)." In Wärmeübertragung A-Z. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-642-56940-1_41.

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Jain, Sudhir Ranjan, Bhooshan S. Paradkar, and Shashikumar M. Chitre. "Low Reynolds Number Flows." In A Primer on Fluid Mechanics with Applications. Springer International Publishing, 2022. http://dx.doi.org/10.1007/978-3-031-20487-6_6.

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Pozrikidis, C. "High-Reynolds-number flow." In Fluid Dynamics. Springer US, 2016. http://dx.doi.org/10.1007/978-1-4899-7991-9_10.

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Pozrikidis, C. "Low-Reynolds-number flow." In Fluid Dynamics. Springer US, 2016. http://dx.doi.org/10.1007/978-1-4899-7991-9_9.

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Pozrikidis, Constantine. "High Reynolds Number Flow." In Fluid Dynamics. Springer US, 2009. http://dx.doi.org/10.1007/978-0-387-95871-2_10.

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Pozrikidis, Constantine. "Low Reynolds Number Flow." In Fluid Dynamics. Springer US, 2009. http://dx.doi.org/10.1007/978-0-387-95871-2_9.

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Streszczenia konferencji na temat "Reynolds's number"

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Pavlíček, Petr. "Local Reynolds number." In 38TH MEETING OF DEPARTMENTS OF FLUID MECHANICS AND THERMODYNAMICS. AIP Publishing, 2019. http://dx.doi.org/10.1063/1.5114763.

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AULEHIA, FELIX. "Pseudo Reynolds number trends." In 5th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-2612.

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Wang, Shu, Yu Zhou, and Md Mahbub Alam. "Effects of Reynolds Number and Turbulent Intensity on a Low Reynolds Number Airfoil." In 32nd AIAA Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-2018.

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Uruba, Václav. "On Reynolds number physical interpretation." In 37TH MEETING OF DEPARTMENTS OF FLUID MECHANICS AND THERMODYNAMICS. Author(s), 2018. http://dx.doi.org/10.1063/1.5049926.

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DRELA, MARK. "Transonic low Reynolds number airfoils." In 9th Applied Aerodynamics Conference. American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-3337.

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Albagli, R. C., L. B. Souza, and A. O. Nieckele. "Reynolds Number Influence on Wax Deposition." In OTC Brasil. Offshore Technology Conference, 2017. http://dx.doi.org/10.4043/28053-ms.

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Laster, M., Egon Stanewsky, D. Sinclair, and W. Sickles. "Reynolds number scaling at transonic speeds." In 20th AIAA Advanced Measurement and Ground Testing Technology Conference. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-2878.

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Brody, J. P., and P. Yager. "Low Reynolds Number Micro-Fluidic Devices." In 1996 Solid-State, Actuators, and Microsystems Workshop. Transducer Research Foundation, Inc., 1996. http://dx.doi.org/10.31438/trf.hh1996.25.

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MARCHMAN, III, J., EDWARD ROBERTSON, and HOWARD EMSLEY. "Rain effects at low Reynolds number." In 25th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-258.

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Bourgoyne, Dwayne A., Carolyn Q. Judge, and Joshua M. Hamel. "Hydrofoil Testing At High Reynolds Number." In SNAME 26th American Towing Tank Conference. SNAME, 2001. http://dx.doi.org/10.5957/attc-2001-015.

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Lifting surfaces are used both for propulsion and control of sea vessels and must meet performance criteria such as lift, drag, and (in some military applications) hydroacoustic noise limits. Design tools suitable to predict such criteria must handle complex flow phenomena and manage the wide range of flow scales inherent in marine applications (Reynolds numbers ~10^8). To date, the development of such tools has been limited by the lack of controlled experimental data in this high Reynolds numbers range. Lifting surface flow is the focus of current high Reynolds number experiments involving a
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Raporty organizacyjne na temat "Reynolds's number"

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Smits, Alexander J. High Reynolds Number Turbulence. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada499452.

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Smits, Alexander J. High Reynolds Number Turbulence. Defense Technical Information Center, 2007. http://dx.doi.org/10.21236/ada465164.

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Wu, K. C. Reynolds Number in MAGCOOL Subcooler. Office of Scientific and Technical Information (OSTI), 1996. http://dx.doi.org/10.2172/1119229.

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Ayoul-Guilmard, Q., S. Ganesh, M. Nuñez, et al. D5.3 Report on theoretical work to allow the use of MLMC with adaptive mesh refinement. Scipedia, 2021. http://dx.doi.org/10.23967/exaqute.2021.2.002.

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This documents describes several studies undertaken to assess the applicability of MultiLevel Monte Carlo (MLMC) methods to problems of interest; namely in turbulent fluid flow over civil engineering structures. Several numerical experiments are presented wherein the convergence of quantities of interest with mesh parameters are studied at different Reynolds’ numbers and geometries. It was found that MLMC methods could be used successfully for low Reynolds’ number flows when combined with appropriate Adaptive Mesh Refinement (AMR) strategies. However, the hypotheses for optimal MLMC performanc
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Bandyopadhyay, P. R., and M. Gad-el-Hak. Reynolds Number Effects in Wall-Bounded Turbulent Flows. Defense Technical Information Center, 1994. http://dx.doi.org/10.21236/ada637054.

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Knight, Doyle D., and Hadassah Naiman. Towards High-Reynolds Number Quiet Flow in Hypersonic Tunnels. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada498212.

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Gimelsheim, N., J. Duncan, T. Lilly, S. Gimelshein, A. Ketsdever, and I. Wysong. Surface Roughness Effects in Low Reynolds Number Channel Flows. Defense Technical Information Center, 2006. http://dx.doi.org/10.21236/ada454769.

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Gopalarothnam, Ashok, and Gregory Z. McGowan. Numerical Study of Unsteady Low-Reynolds Number Wing Performance. Defense Technical Information Center, 2008. http://dx.doi.org/10.21236/ada479418.

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Schneider, Steven P. Towards High-Reynolds-Number Quiet Flow in Hypersonic Wind Tunnels. Defense Technical Information Center, 2009. http://dx.doi.org/10.21236/ada500049.

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Glauser, Mark N., and Jacques Lewalle. Closed-Loop Control for High Reynolds Number Turbulent Compressible Jets. Defense Technical Information Center, 2011. http://dx.doi.org/10.21236/ada566128.

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