Relevant bibliographies by topics / Low Reynolds numbers

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

Academic literature on the topic 'Low Reynolds numbers'

Author: Grafiati
Published: 4 June 2021
Last updated: 6 September 2023

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Journal articles on the topic "Low Reynolds numbers"

1

Brody, J. P., P. Yager, R. E. Goldstein, and R. H. Austin. "Biotechnology at low Reynolds numbers." Biophysical Journal 71, no. 6 (1996): 3430–41. http://dx.doi.org/10.1016/s0006-3495(96)79538-3.

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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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Marchman, J. F. "Aerodynamic testing at low Reynolds numbers." Journal of Aircraft 24, no. 2 (1987): 107–14. http://dx.doi.org/10.2514/3.45426.

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SWAIN, F. C., and N. EPSTEIN. "ORIFICE METERING AT LOW REYNOLDS NUMBERS." Chemical Engineering Communications 82, no. 1 (1989): 193–201. http://dx.doi.org/10.1080/00986448908940641.

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Barrero-Gil, A., A. Sanz-Andrés, and M. Roura. "Transverse galloping at low Reynolds numbers." Journal of Fluids and Structures 25, no. 7 (2009): 1236–42. http://dx.doi.org/10.1016/j.jfluidstructs.2009.07.001.

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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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Torres, Gabriel E., and Thomas J. Mueller. "Low Aspect Ratio Aerodynamics at Low Reynolds Numbers." AIAA Journal 42, no. 5 (2004): 865–73. http://dx.doi.org/10.2514/1.439.

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Li, Lin, Wei Tan, Jianshe Zhang, Ge Han, and Yanfeng Zhang. "Unsteady Effects of Wake on Downstream Rotor at Low Reynolds Numbers." Energies 15, no. 18 (2022): 6692. http://dx.doi.org/10.3390/en15186692.

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In a compressor, the periodic wake is an inherently unsteady phenomenon that affects the downstream flow conditions and loading distribution. Thus, understanding the physical mechanisms of these unsteady effects is important for eliminating flow losses and improving compressor performance, particularly at low Reynolds numbers. To understand the influence of the upstream wake on the downstream flow field structure, this paper describes numerical simulations of a one-stage high-pressure compressor at altitudes of 10–20 km. The influence of the wake on rotor flow blockage at different Reynolds nu
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Hu, Hui, Masatoshi Tamai, and Jeffery T. Murphy. "Flexible-Membrane Airfoils at Low Reynolds Numbers." Journal of Aircraft 45, no. 5 (2008): 1767–78. http://dx.doi.org/10.2514/1.36438.

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Hu, Hui, and Masatoshi Tamai. "Bioinspired Corrugated Airfoil at Low Reynolds Numbers." Journal of Aircraft 45, no. 6 (2008): 2068–77. http://dx.doi.org/10.2514/1.37173.

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Dissertations / Theses on the topic "Low Reynolds numbers"

1

Ishimoto, Kenta. "Hydrodynamics of squirming locomotion at low Reynolds numbers." 京都大学 (Kyoto University), 2015. http://hdl.handle.net/2433/199079.

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Heathcote, Samuel Francis. "Flexible flapping airfoil propulsion at low Reynolds numbers." Thesis, University of Bath, 2006. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.432380.

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Sathaye, Sagar Sanjeev. "Lift distributions on low aspect ratio wings at low Reynolds numbers." Link to electronic thesis, 2004. http://www.wpi.edu/Pubs/ETD/Available/etd-0427104-091112.

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Thesis (M.S.)--Worcester Polytechnic Institute.<br>Keywords: Low Reynolds Number; Micro Air Vehicle; Low Aspect Ratio; Spanwise pressure measurements; Spanwise Lift Distributions. Includes bibliographical references (p. 84-85).
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Papangelou, Ares. "Vortex shedding from slender cones at low Reynolds numbers." Thesis, University of Cambridge, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.387050.

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Garcia, Gonzalez Jesus. "Numerical analysis of fluid motion at low Reynolds numbers." Thesis, University of Manchester, 2017. https://www.research.manchester.ac.uk/portal/en/theses/numerical-analysis-of-fluid-motion-at-low-reynolds-numbers(4cf30194-0155-439d-879a-c49787549e8c).html.

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At low Reynolds number flows, the effect of inertia becomes negligible and the fluid motion is dominated by the effect of viscous forces. Understanding of the behaviour of low Reynolds number flows underpins the prediction of the motion of microorganisms and particle sedimentation as well as the development of micro-robots that could potentially swim inside the human body to perform targeted drug/cell delivery and non-invasive microsurgery. The work in this thesis focuses on developing an understanding in the mathematical analysis of objects moving at low Reynolds numbers. A boundary element i
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Abtahi, Ali A. "Aspect ratio effects on wings at low Reynolds numbers." Diss., Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/52330.

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In this study the primary objective was to determine the effect of aspect ratio in particular and in general the effect of three dimensionality on the flow around wings at low Reynolds numbers. It was seen that the effects observed at high Reynolds number are also present in this Re range. There is the usual increase in lift slope and this increase can even be predicted with reasonable accuracy using Prandtl's lifting line theory. In addition to the change in lift slope the zero lift angle of attack was also influenced by the aspect ratio. Through flow visualization it was ascertained that t
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SBRAGAGLIA, MAURO. "Modelling fluid dynamics at high and low reynolds numbers." Doctoral thesis, Università degli Studi di Roma "Tor Vergata", 2004. http://hdl.handle.net/2108/202683.

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Lo studio sviluppato in questa tesi di dottorato è rivolto principalmente alla comprensione di proprietà di fluidi su grande e piccola scala. Tutti i tentativi di descrizione incontrano sfortunatamente aspetti non lineari nelle equazioni del moto che sono difficilmente trattabili. Questo è il motivo per cui modellizazioni computazionali e teoriche possono essere di grande aiuto. Per quanto riguarda l’aspetto teorico, una esplorazione sistematica delle proprietà statistiche di un fluido turbolento a piccola scala è stata effettuata su modelli deterministici noti come modelli a Shell. L’approccio con
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Tregidgo, Luke. "Low aspect-ratio rigid, flexible and membrane wings at low Reynolds numbers." Thesis, University of Bath, 2013. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.577740.

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The interest in developing small, payload-carrying Micro Air Vehicles (MAVs) with a maximum linear dimension of six inches or below is as strong as ever, with both military and civilian bodies interested in the remote sensing capabilities such a vehicle would provide. However significant challenges remain in developing such aircraft and the research presented here addresses specific issues in the field of fluid-structure interactions for flexible wings. Wind tunnel tests were conducted on rectangular, aspect-ratio-two, rigid and flexible wings (including membrane wings) in an open-jet, closed-
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Jones, Robin. "Aerodynamics of biplane and tandem wings at low Reynolds numbers." Thesis, University of Bath, 2016. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.693328.

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Overcoming the difficulties associated with low Reynolds number flows has recently become a primary goal for aerodynamicists due to the growing importance of micro air vehicles (MAVs). The limiting size requirement of a six-inch wing span for MAVs combined with their inherent tendency to suffer stall due to gusts makes this significantly more challenging. The use of two-wing configurations, inspired by historical aircraft, could prove to be an effective method of overcoming this limitation. This thesis is primarily concerned with the fundamental aerodynamics associated with biplane and tandem
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Pitt, Ford Charles William. "Unsteady aerodynamic forces on accelerating wings at low Reynolds numbers." Thesis, University of Cambridge, 2013. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.608219.

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Books on the topic "Low Reynolds numbers"

1

Kohr, Mirela. Viscous incompressible flow for low Reynolds numbers. WIT, 2004.

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Morgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.

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Morgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.

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Morgan, Harry L. A study of high-lift airfoils at high Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1989.

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Borthwick, A. G. L. Jet-forced flow inside a circle at very low Reynolds numbers. University of Salford Department of Civil Engineering, 1988.

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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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Chan, Y. Y. Analysis of experimental data for cast 10-2/DOA 2 supercritical airfoil at low Reynolds numbers and application to high Reynolds number flow. National Research Council of Canada, 1989.

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Hicks, R. M. An evaluation of three two-dimensional computational fluid dynamics codes including low Reynolds numbers and transonic Mach numbers. Ames Research Center, 1991.

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S, Walker Betty, Millard Betty F, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Experimental results for the Eppler 387 airfoil at low Reynolds numbers in the Langley Low-Turbulence Pressure Tunnel. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

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C, Yu James, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. New technique for experimental generation of two-dimensional blade-vortex interaction at low Reynolds numbers. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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Book chapters on the topic "Low Reynolds numbers"

1

Pozrikidis, C. "Flow at Low Reynolds Numbers." In Fluid Dynamics. Springer US, 2001. http://dx.doi.org/10.1007/978-1-4757-3323-5_9.

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Sadhal, S. S., P. S. Ayyaswamy, and J. N. Chung. "Transport at Low Reynolds Numbers." In Transport Phenomena with Drops and Bubbles. Springer New York, 1997. http://dx.doi.org/10.1007/978-1-4612-4022-8_3.

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Baranyi, L. "Orbiting Cylinder at Low Reynolds Numbers." In IUTAM Symposium on Unsteady Separated Flows and their Control. Springer Netherlands, 2009. http://dx.doi.org/10.1007/978-1-4020-9898-7_13.

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Zeytounian, Radyadour Kh. "The Limit of Very Low Reynolds Numbers." In Theory and Applications of Viscous Fluid Flows. Springer Berlin Heidelberg, 2004. http://dx.doi.org/10.1007/978-3-662-10447-7_6.

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Render, P. M., J. L. Stollery, and B. R. Williams. "Aerofoils at Low Reynolds Numbers—Prediction and Experiment." In Numerical and Physical Aspects of Aerodynamic Flows III. Springer New York, 1986. http://dx.doi.org/10.1007/978-1-4612-4926-9_9.

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Wu, Xiao Z. "Free Thermal Convection In Low Temperature Helium Gas." In Flow at Ultra-High Reynolds and Rayleigh Numbers. Springer New York, 1998. http://dx.doi.org/10.1007/978-1-4612-2230-9_14.

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Segawa, T., M. Sano, A. Naert, and J. A. Glazier. "High Rayleigh Number Turbulence of a Low Prandtl Number Fluid." In Flow at Ultra-High Reynolds and Rayleigh Numbers. Springer New York, 1998. http://dx.doi.org/10.1007/978-1-4612-2230-9_16.

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McGhee, Robert J., and Betty S. Walker. "Performance Measurements of an Airfoil at Low Reynolds Numbers." In Lecture Notes in Engineering. Springer Berlin Heidelberg, 1989. http://dx.doi.org/10.1007/978-3-642-84010-4_11.

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Papangelou, A. "Vortex Shedding from Slender Cones at Low Reynolds Numbers." In Bluff-Body Wakes, Dynamics and Instabilities. Springer Berlin Heidelberg, 1993. http://dx.doi.org/10.1007/978-3-662-00414-2_77.

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Höfler, K., and S. Schwarzer. "The Structure of Bidisperse Suspensions at Low Reynolds Numbers." In Multifield Problems. Springer Berlin Heidelberg, 2000. http://dx.doi.org/10.1007/978-3-662-04015-7_5.

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Conference papers on the topic "Low Reynolds numbers"

1

MARCHMAN, J. "Aerodynamic testing at low Reynolds numbers." In 14th Aerodynamic Testing Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-779.

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Shields, Matthew C., and Kamran Mohseni. "Roll Stability Regimes at Low Reynolds Numbers." In AIAA Guidance, Navigation, and Control Conference. American Institute of Aeronautics and Astronautics, 2015. http://dx.doi.org/10.2514/6.2015-1551.

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Selig, Michael, James Guglielmo, Andy Broern, and Philippe Giguere. "Experiments on airfoils at low Reynolds numbers." In 34th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1996. http://dx.doi.org/10.2514/6.1996-62.

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Muramatsu, Akinori, and Tatsuo Motohashi. "Two Dimensional Jet at Low Reynolds Numbers." In ASME/JSME 2007 5th Joint Fluids Engineering Conference. ASMEDC, 2007. http://dx.doi.org/10.1115/fedsm2007-37221.

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A numerical simulation of two-dimensional jets was carried out using a SOLA method. The two-dimensional jets were discharged from a slit in a wall at Reynolds numbers below 50. The difference between the calculated flow fields and those of the Bickley jet is due to the non-uniformity of the pressure field near the jet exit at the wall. The jet spreads faster than the Bickley jet. The decay of the streamwise velocity on the center line is more rapid than that of the Bickley jet. The streamwise velocity profile is different from that of the Bickley jet, and a reversed flow is generated in the ou
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Jones, Anya, and Holger Babinsky. "Leading Edge Flaps at Low Reynolds Numbers." In 46th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-424.

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Cleaver, David, Zhi-Jin Wang, and Ismet Gursul. "Oscillating Flexible Wings at Low Reynolds Numbers." In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-674.

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Moriche, Manuel, Alejandro Gonzalo, Oscar Flores, and Manuel Garcia-Villalba. "Fast transverse maneuvers at low Reynolds numbers." In AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-0640.

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Brandt, John, and Michael Selig. "Propeller Performance Data at Low Reynolds Numbers." In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-1255.

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Selig, Michael, Robert Deters, and Gregory Wiliamson. "Wind Tunnel Testing Airfoils at Low Reynolds Numbers." In 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-875.

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Hatton, Ross, and Howie Choset. "Kinematic Cartography for Locomotion at Low Reynolds Numbers." In Robotics: Science and Systems 2011. Robotics: Science and Systems Foundation, 2011. http://dx.doi.org/10.15607/rss.2011.vii.017.

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Reports on the topic "Low Reynolds numbers"

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Reed, Helen L. Three-Dimensional Unsteady Separation at Low Reynolds Numbers. Defense Technical Information Center, 1990. http://dx.doi.org/10.21236/ada225167.

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Jamison, Andrew, and Andrew D. Ketsdever. Performance Comparisons of Underexpanded Orifices and DeLaval Nozzles at Low Reynolds Numbers. Defense Technical Information Center, 2002. http://dx.doi.org/10.21236/ada406211.

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Ketsdever, Andrew D., Michael T. Clabough, Sergey F. Gimelshein, and Alina Alexeenko. Experimental and Numerical Determination of Micropropulsion Device Efficiencies at Low Reynolds Numbers. Defense Technical Information Center, 2004. http://dx.doi.org/10.21236/ada432073.

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Mueller, Thomas J., and Gabriel E. Torres. Aerodynamics of Low Aspect Ratio Wings at Low Reynolds Numbers with Applications to Micro Air Vehicle Design and Optimization. Defense Technical Information Center, 2001. http://dx.doi.org/10.21236/ada397533.

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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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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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Ol, Michael V. Unsteady Low-Reynolds Number Aerodynamics for Micro Air Vehicles (MAVs). Defense Technical Information Center, 2007. http://dx.doi.org/10.21236/ada472788.

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Bianchi, J. Christopher. Velocity measurements of low Reynolds number tube flow using fiber-optic technology. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/10140118.

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Bianchi, J. C. Velocity measurements of low Reynolds number tube flow using fiber-optic technology. Office of Scientific and Technical Information (OSTI), 1993. http://dx.doi.org/10.2172/6625783.

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