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Journal articles on the topic 'Reynolds's number'

Author: Grafiati

Published: 3 June 2025

Last updated: 31 July 2025

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1

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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2

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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3

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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4

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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5

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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6

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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7

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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8

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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9

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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10

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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11

Franziska, Konig, Zanoun El-Sayed, Jehring Lothar, and Egbers Christoph. "1226 THE COLAPIPE - A HIGH REYNOLDS NUMBER PIPE TEST FACILITY." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1226–1_—_1226–6_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1226-1_.

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12

Shu, Wang, Zhou Yu, and Alam Md.Mahbub. "1225 EFFECT OF TURBULENCE INTENSITY ON THE LOW REYNOLDS NUMBER AIRFOILWAKE." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1225–1_—_1225–6_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1225-1_.

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13

Hsiao, Fei-Bin, Di-Bao Wang, Yi-Chung Liu, et al. "The Low Reynolds Number Wing Aerodynamics and Micro Aerial Vehicles Development." Reference Collection of Annual Meeting 2004.8 (2004): 13–17. http://dx.doi.org/10.1299/jsmemecjsm.2004.8.0_13.

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14

Funaki, Jiro, Motohide Hisada, and Katsuya Hirata. "Aspect-Ratio and Reynolds-number Effect On Cross-Flow Impellers(Fluid Machinery)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 507–12. http://dx.doi.org/10.1299/jsmeicjwsf.2005.507.

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15

Kahalerras, H., Y. Malécot, Y. Gagne, and B. Castaing. "Intermittency and Reynolds number." Physics of Fluids 10, no. 4 (1998): 910–21. http://dx.doi.org/10.1063/1.869613.

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16

Horiguchi, Hironori, Daisuke Yumiba, Yoshinobu Tsujimoto, Masaaki Sakagami, and Shigeo Tanaka. "Reynolds Number Effect on Regenerative Pump Performance in Low Reynolds Number Range." International Journal of Fluid Machinery and Systems 1, no. 1 (2008): 101–8. http://dx.doi.org/10.5293/ijfms.2008.1.1.101.

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17

KLOZINSKI, ARKADIUSZ. "Evaluation of the Reynolds number in rheological measurements of polyethylene." Polimery 55, no. 07/08 (2010): 575–81. http://dx.doi.org/10.14314/polimery.2010.575.

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18

x, Asaduzzaman, and Md Lutfor Rahman. "Friction Factor Diagram on Turbulent Flow by Different Reynolds Number in Small Pipes." International Journal of Scientific Engineering and Research 7, no. 1 (2019): 58–63. https://doi.org/10.70729/ijser18522.

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19

Seo, Il Won. "Flow Characteristics According to Velocity Conditions of Cylinder Boundary Under Low Reynolds Number." Journal of the Korean Society of Civil Engineers 33, no. 6 (2013): 2267. http://dx.doi.org/10.12652/ksce.2013.33.6.2267.

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20

Zheng, Tinghui, S. K. Tang, and Baoling Fei. "ON THE FORCES AND STROUHAL NUMBERS IN THE LOW REYNOLDS NUMBER WAKES OF TWO CYLINDERS IN TANDEM." Transactions of the Canadian Society for Mechanical Engineering 33, no. 3 (2009): 349–60. http://dx.doi.org/10.1139/tcsme-2009-0025.

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The flow around two circular cylinders of equal diameter in tandem arrangement was investigated numerically using the finite volume method in the present study. The code was validated by comparison with previous works at the Reynolds number of 200. A systematic investigation of the relationships of Strouhal number and the aerodynamic forces with cylinder separation and Reynolds number was done. Results demonstrate not only the important combined effects cylinder separation and Reynolds number on the wake aerodynamics, but also on the relative strengths of the forces acting on the two cylinders

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21

Chen, Hao, Zi-Ren Wang, Qi-Fan Zhang, Xiao-Yuan Zhang, and Lian-Jie Yue. "On the Reynolds-Number Sensitivity of Inlet Flow at Mach Numbers Beyond 7." AIAA Journal 60, no. 3 (2022): 1978–82. http://dx.doi.org/10.2514/1.j061157.

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22

Iwasawa, Yuzuru, Yutaka Abe, Akiko Kaneko, et al. "ICONE23-1950 NUMERICAL STUDY ON INFLUENCE OF OHNESORGE NUMBER AND REYNOLDS NUMBER ON THE JET BREAKUP BEHAVIOR USING THE LATTICE BOLTZMANN METHOD." Proceedings of the International Conference on Nuclear Engineering (ICONE) 2015.23 (2015): _ICONE23–1—_ICONE23–1. http://dx.doi.org/10.1299/jsmeicone.2015.23._icone23-1_444.

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23

Jayathilake, W. A. R. D., and J. I. Abeygoonewardene. "Estimation of CLARK Y-14 Airfoil’s Lift Hysteresis in Low-Speed Flow." KDU Journal of Multidisciplinary Studies 6, no. 1 (2024): 55–61. http://dx.doi.org/10.4038/kjms.v6i1.109.

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A phenomenon called hysteresis is responsible for the difference in the separation and the reattachment angles of an airfoil which is seen within the vicinity of the stalling angle of attack. The reason for this is the difference in the expected lift distribution of an airfoil for a particular angle of attack when recovery from stall is achieved. This leads to asymmetric flow parameters around a body even when the boundaries remain symmetric. Empirical results were obtained for a two-dimensional Clark Y-14 airfoil by varying the angle of attack for different Reynold’s numbers in order to estim

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24

SULAIMAN, Taufik, Makoto SATO, Satoshi SEKIMOTO, Taku NONOMURA, Akira Oyama, and Kozo FUJII. "S052034 Multi-Objective Design Exploration of DBD Plasma Actuator for Low Reynolds Number Application." Proceedings of Mechanical Engineering Congress, Japan 2013 (2013): _S052034–1—_S052034–5. http://dx.doi.org/10.1299/jsmemecj.2013._s052034-1.

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25

Leschziner, M. A. "Simulating Flow Separation from Continuous Surfaces : Routes to Overcoming the Reynolds Number Barrier(1)." Proceedings of the Fluids engineering conference 2007 (2007): A1—A17. http://dx.doi.org/10.1299/jsmefed.2007.a1.

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26

Leschziner, M. A. "Simulating Flow Separation from Continuous Surfaces : Routes to Overcoming the Reynolds Number Barrier(2)." Proceedings of the Fluids engineering conference 2007 (2007): C1—C17. http://dx.doi.org/10.1299/jsmefed.2007.c1.

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27

Furuichi, Noriyuki, Hiroshi Sato, Yoshiya Terao, and Masaki Takamoto. "ICONE15-10209 A FACILITY WITH HIGH REYNOLDS NUMBER FOR CALIBRATION OF A FEEDWATER FLOWMETER." Proceedings of the International Conference on Nuclear Engineering (ICONE) 2007.15 (2007): _ICONE1510. http://dx.doi.org/10.1299/jsmeicone.2007.15._icone1510_101.

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28

J. J., Miau, Fang C. H., Chen M. C., and Wang C. T. "1032 FLOW OVER A CIRCULAR CYLINDER AT PRE-CRITICAL REYNOLDS NUMBERS." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1032–1_—_1032–8_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1032-1_.

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29

Yuta, Yamaguchi, Ohtake Tomohisa, and Muramatsu Akinori. "1201 PRESSURE DISTRIBUTION ON A NACA0012 AIRFOIL AT LOW REYNOLDS NUMBERS." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2013.4 (2013): _1201–1_—_1201–5_. http://dx.doi.org/10.1299/jsmeicjwsf.2013.4._1201-1_.

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30

DÜTSCH, H., F. DURST, S. BECKER, and H. LIENHART. "Low-Reynolds-number flow around an oscillating circular cylinder at low Keulegan–Carpenter numbers." Journal of Fluid Mechanics 360 (April 10, 1998): 249–71. http://dx.doi.org/10.1017/s002211209800860x.

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Time-averaged LDA measurements and time-resolved numerical flow predictions were performed to investigate the laminar flow induced by the harmonic in-line oscillation of a circular cylinder in water at rest. The key parameters, Reynolds number Re and Keulegan–Carpenter number KC, were varied to study three parameter combinations in detail. Good agreement was observed for Re=100 and KC=5 between measurements and predictions comparing phase-averaged velocity vectors. For Re=200 and KC=10 weakly stable and non-periodic flow patterns occurred, which made repeatable time-averaged measurements impos

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31

Martín, Mariano, Francisco J. Montes, and Miguel A. Galán. "Approximate theoretical solution for the Sherwood number of oscillating bubbles at different Reynolds numbers." Chemical Engineering and Processing: Process Intensification 49, no. 3 (2010): 245–54. http://dx.doi.org/10.1016/j.cep.2010.01.012.

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32

Drela, Mark. "Transonic low-Reynolds number airfoils." Journal of Aircraft 29, no. 6 (1992): 1106–13. http://dx.doi.org/10.2514/3.46292.

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33

Traub, Lance W., and Cory Coffman. "Efficient Low-Reynolds-Number Airfoils." Journal of Aircraft 56, no. 5 (2019): 1987–2003. http://dx.doi.org/10.2514/1.c035515.

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34

Najafi, Ali, and Ramin Golestanian. "Propulsion at low Reynolds number." Journal of Physics: Condensed Matter 17, no. 14 (2005): S1203—S1208. http://dx.doi.org/10.1088/0953-8984/17/14/009.

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35

Berti, Luca, Laetitia Giraldi, and Christophe Prud’homme. "Swimming at low Reynolds number." ESAIM: Proceedings and Surveys 67 (2020): 46–60. http://dx.doi.org/10.1051/proc/202067004.

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We address the swimming problem at low Reynolds number. This regime, which is typically used for micro-swimmers, is described by Stokes equations. We couple a PDE solver of Stokes equations, derived from the Feel++ ﬁnite elements library, to a quaternion-based rigid-body solver. We validate our numerical results both on a 2D exact solution and on an exact solution for a rotating rigid body respectively. Finally, we apply them to simulate the motion of a one-hinged swimmer, which obeys to the scallop theorem.

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36

Riley, N., and R. Vasantha. "Unsteady high-Reynolds-number flows." Journal of Fluid Mechanics 205, no. -1 (1989): 243. http://dx.doi.org/10.1017/s0022112089002028.

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37

WILLIAMSON, N., N. SRINARAYANA, S. W. ARMFIELD, G. D. McBAIN, and W. LIN. "Low-Reynolds-number fountain behaviour." Journal of Fluid Mechanics 608 (July 11, 2008): 297–317. http://dx.doi.org/10.1017/s0022112008002310.

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Experimental evidence for previously unreported fountain behaviour is presented. It has been found that the first unstable mode of a three-dimensional round fountain is a laminar flapping motion that can grow to a circling or multimodal flapping motion. With increasing Froude and Reynolds numbers, fountain behaviour becomes more disorderly, exhibiting a laminar bobbing motion. The transition between steady behaviour, the initial flapping modes and the laminar bobbing flow can be approximately described by a function FrRe2/3=C. The transition to turbulence occurs at Re > 120, independent of

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38

Smits, Alexander J., Beverley J. McKeon, and Ivan Marusic. "High–Reynolds Number Wall Turbulence." Annual Review of Fluid Mechanics 43, no. 1 (2011): 353–75. http://dx.doi.org/10.1146/annurev-fluid-122109-160753.

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39

Golestanian, Ramin, and Armand Ajdari. "Stochastic low Reynolds number swimmers." Journal of Physics: Condensed Matter 21, no. 20 (2009): 204104. http://dx.doi.org/10.1088/0953-8984/21/20/204104.

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40

Boucher, R. F., and C. Mazharoglu. "Low Reynolds number fluidic flowmetering." Journal of Physics E: Scientific Instruments 21, no. 10 (1988): 977–89. http://dx.doi.org/10.1088/0022-3735/21/10/015.

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41

Thompson, H. Doyle, Brent W. Webb, and Joe D. Hoffman. "The cell Reynolds number myth." International Journal for Numerical Methods in Fluids 5, no. 4 (1985): 305–10. http://dx.doi.org/10.1002/fld.1650050402.

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42

Yasuda, Takahiro, Keita Fukui, Keiji Matsuo, Hisato Minagawa, and Ryo Kurimoto. "Effect of the Reynolds Number on the Performance of a NACA0012 Wing with Leading Edge Protuberance at Low Reynolds Numbers." Flow, Turbulence and Combustion 102, no. 2 (2018): 435–55. http://dx.doi.org/10.1007/s10494-018-9978-3.

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43

Yamada, Shunsuke, Hirotatsu Sagawa, Shinsuke Okamoto, and Shinji Honami. "A Behavior of Backward Facing Step Flow in Low Reynolds Number(Swirling Flow and Separation)." Proceedings of the International Conference on Jets, Wakes and Separated Flows (ICJWSF) 2005 (2005): 709–14. http://dx.doi.org/10.1299/jsmeicjwsf.2005.709.

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44

Jain, Suhas S., Neha Tyagi, R. Surya Prakash, R. V. Ravikrishna, and Gaurav Tomar. "Secondary breakup of drops at moderate Weber numbers: Effect of Density ratio and Reynolds number." International Journal of Multiphase Flow 117 (August 2019): 25–41. http://dx.doi.org/10.1016/j.ijmultiphaseflow.2019.04.026.

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45

Park, Jongmyung, Matt Goodro, Phil Ligrani, Mike Fox, and Hee-Koo Moon. "Separate Effects of Mach Number and Reynolds Number on Jet Array Impingement Heat Transfer." Journal of Turbomachinery 129, no. 2 (2006): 269–80. http://dx.doi.org/10.1115/1.2437774.

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Limited available data suggest a substantial impact of Mach number on the heat transfer from an array of jets impinging on a surface at fixed Reynolds number. Many jet array heat transfer correlations currently in use are based on tests in which the jet Reynolds number was varied by varying the jet Mach number. Hence, this data may be inaccurate for high Mach numbers. Results from the present study are new and innovative because they separate the effects of jet Reynolds number and jet Mach number for the purposes of validating and improving correlations that are currently in use. The present s

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46

Dsouza, Brian, Andrea Sciacchitano, and W. Yu. "Reynolds Number Independence In An Urban Street Canyon Using 3D Robotic Particle Tracking Velocimetry." Proceedings of the International Symposium on the Application of Laser and Imaging Techniques to Fluid Mechanics 21 (July 8, 2024): 1–14. http://dx.doi.org/10.55037/lxlaser.21st.171.

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The Reynolds number in an Urban Street Canyon is a difficult parameter to match between reduced-scale experiments and full-scale measurements. It is possible to overcome this mismatch in Reynolds numbers by satisfying the Reynolds number independence criterion, which states that above a certain critical Reynolds number, the flow field remains invariant with increasing Reynolds numbers. For an urban canyon with an aspect ratio 1, this critical Reynolds number is often reported to be 12000 for the mean flow quantities. This critical Reynolds number, however, is not applicable for higher-order qu

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47

Ali Sabri Abbas and Ayad Ali Mohammed. "Enhancement Of Plate-Fin Heat Exchanger Performance with Aid of Various Types of Fin Configurations: A Review." Journal of Advanced Research in Fluid Mechanics and Thermal Sciences 99, no. 2 (2022): 48–66. http://dx.doi.org/10.37934/arfmts.99.2.4866.

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This study is a review of recent studies on heat transfer enhancement in plate fin-heat exchangers (PFHE) with plain and offset (OSF) fins. Thermal designing parameters such as the coefficient of heat transfer, Nusselt number, hydraulic diameter, Colburn factor (j), friction factor (f) and Reynold's number of PFHE was presented in this review for both straight and offset types. According to the results, by replacing plain fins into OSF, the pressure increases because of the increasing of f-factor, while there is a significant increase in Nusselt number and then the heat transfer. The j & f

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48

Marchman, J. F., Edward A. Robertson, and Howard T. Emsley. "Rain effects at low Reynolds number." Journal of Aircraft 24, no. 9 (1987): 638–44. http://dx.doi.org/10.2514/3.45489.

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49

Traub, Lance W. "Drag Extrapolation to Higher Reynolds Number." Journal of Aircraft 46, no. 4 (2009): 1458–61. http://dx.doi.org/10.2514/1.43952.

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50

Glass, O., and T. Horsin. "Lagrangian controllability at low Reynolds number." ESAIM: Control, Optimisation and Calculus of Variations 22, no. 4 (2016): 1040–53. http://dx.doi.org/10.1051/cocv/2016032.

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