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Dissertations / Theses on the topic 'Reynolds's No'

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Published: 3 June 2025

Last updated: 31 July 2025

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1

Роговий, Андрій Сергійович. "Розробка теорії та методів розрахунку вихорокамерних нагнітачів". Thesis, Харківський національний автомобільно-дорожній університет, 2017. http://repository.kpi.kharkov.ua/handle/KhPI-Press/29275.

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Дисертація на здобуття наукового ступеня доктора технічних наук за спеціальністю 05.05.17 – гідравлічні машини та гідропневмоагрегати. – Національний технічний університет "Харківський політехнічний інститут", Харків, 2017. У дисертаційній роботі розв'язано науково-практичну проблему підвищення техніко-економічної ефективності гідравлічних і пневматичних нагнітачів, що перекачують рідини в несприятливих умовах експлуатації або гетерогенні середовища, за рахунок розробки і використання принципово нового типу струминних нагнітачів відцентрової дії. Їх конструкція не містить рухомих механічних

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2

Роговий, Андрій Сергійович. "Розробка теорії та методів розрахунку вихорокамерних нагнітачів". Thesis, НТУ "ХПІ", 2017. http://repository.kpi.kharkov.ua/handle/KhPI-Press/29269.

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Дисертація на здобуття наукового ступеня доктора технічних наук за спеціальністю 05.05.17 – гідравлічні машини та гідропневмоагрегати. – Національний технічний університет "Харківський політехнічний інститут", Харків, 2017. У дисертаційній роботі розв'язано науково-практичну проблему підвищення техніко-економічної ефективності гідравлічних і пневматичних нагнітачів, що перекачують рідини в несприятливих умовах експлуатації або гетерогенні середовища, за рахунок розробки і використання принципово нового типу струминних нагнітачів відцентрової дії. Їх конструкція не містить рухомих механічних ч

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3

Turnage, Amy. "Reynolds Bath House." VCU Scholars Compass, 2014. http://scholarscompass.vcu.edu/etd/3451.

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Abstract: This project explores the ritual of leisure, social interaction, and reflection in a democratic* space. Water is the universal experience. The program for this site examines the ritual of bathing and the role of intimacy within a public domain. *democratic: absence of hereditary or arbitrary class distinctions or privileges

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4

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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5

Essel, Emmanuel Kwame. "Homogenization of Reynolds equations." Licentiate thesis, Luleå : Luleå University of Technology, 2007. http://epubl.ltu.se/1402-1757/2007/30/.

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6

Garcia, Angèle. "Le syndrome de Reynolds." Bordeaux 2, 1997. http://www.theses.fr/1997BOR2M054.

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7

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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8

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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9

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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10

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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11

Abell, Martha Louise. "Symmetry reduction of Reynold's equation and applications to film lubrication." Diss., Georgia Institute of Technology, 1989. http://hdl.handle.net/1853/28669.

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12

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

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13

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

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14

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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15

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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16

Pietropinto, Sylvain. "Expérience à grands Reynolds cryogéniques : GReC." Université Joseph Fourier (Grenoble), 2002. http://www.theses.fr/2002GRE10089.

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17

Box, Stuart James. "Rotational motion at low Reynolds number." Thesis, University of Bristol, 2015. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.688351.

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Driven cyclic or periodic motion is a recurrent feature of many of the microscopic mechanical systems that support life. For example, fields of cilia, nano-scale hair-like structures, beat together to transport fluids though mammalian tracts. Bacteria and other micro-organisms are able to swim using similar organelles known as flagella, while "molecular motors" provide traction in muscle tissue. These mechanisms rely on the hydrodynamics and statistical mechanics of driven cyclic motion at the micro-scale. The purpose of this thesis is to investigate these principles in an abstract sense, in o

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18

Dandy, David Stewart Leal L. Gary. "Intermediate Reynolds number free-surface flows /." Diss., Pasadena, Calif. : California Institute of Technology, 1987. http://resolver.caltech.edu/CaltechETD:etd-03042008-083806.

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19

Lee, JooHee. "Roger Reynolds' Variation (1988) new concepts of form and sound /." Thesis, connect to online resource. Access restricted to the University of North Texas campus, 2003. http://www.library.unt.edu/theses/open/20033/lee%5Fjoohee/index.htm.

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Thesis (D.M.A.)--University of North Texas, 2003.<br>Accompanied by 4 recitals, recorded June 28, 1999, Sept. 11, 2000, Apr. 15, 2002, and Aug. 8, 2003. Includes bibliographical references and discography (p. 38-40).

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20

Postle, Martin Joseph. "The subject pictures of Sir Joshua Reynolds." Thesis, Birkbeck (University of London), 1990. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.494584.

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21

Carvalho, Isa Diana de Sousa Baptista Morais. "Low reynolds propellers for increased quadcopters endurance." Master's thesis, Universidade da Beira Interior, 2013. http://hdl.handle.net/10400.6/1977.

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With this MSit c. Dissertation in Aeronautical Engineering is intended to contribute to the research and development of long endurance quadcopters. In this dissertation, initially, the topic study is introduced and the principals components (propeller, motor and battery) for greater autonomy quadcopters are described along with the advances made by the aeronautical sector in this strand and the possible applications. Posteriorly, a description of the program used for the analysis of existing propellers and new designs is given, and its validation is performed with the experimental data set of

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22

Ames, Danielle 1974. "Shear flow visualization at high Reynolds Numbers." Thesis, Massachusetts Institute of Technology, 1998. http://hdl.handle.net/1721.1/50478.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Ocean Engineering, 1998.<br>Includes bibliographical references (leaves 92-94).<br>The mechanisms responsible for various disturbances in the wakes of ships have been investigated for some time. Efforts to define and characterize the contributing factors and resulting turbulent wake manifestations conclude that ship length, speed and geometry play integral and interdependent roles. Previous experimentation in the Ocean Engineering Towing Tank at MIT on small scale model ships supplied data for Reynold's Numbers up to ~ 0(106). The

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23

Samson, Ophir. "Low Reynolds number swimming in complex environments." Thesis, Imperial College London, 2010. http://hdl.handle.net/10044/1/5723.

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The study of swimming micro-organisms has been of interest not just to biologists, but also to fluid dynamicists for over a century. As they are rarely in isolation, much interest has been focused on the study of the swimmers’ interaction with their environment. By virtue of the typically small sizes of these organisms and their swimming protocols, the characteristic Reynolds number of the motion of the fluid around them is small. Hence they reside in a Stokes flow regime where viscous forces dominate inertial effects and where far-field interactions (e.g. with nearby walls) can have a signifi

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24

Yu, Tony S. (Tony Sheung). "Elastic tail propulsion at low Reynolds number." Thesis, Massachusetts Institute of Technology, 2007. http://hdl.handle.net/1721.1/38700.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2007.<br>This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.<br>Includes bibliographical references (p. 73-76).<br>A simple way to generate propulsion at low Reynolds number is to periodically oscillate a passive flexible filament. Here we present a macroscopic experimental investigation of such a propulsive mechanism. A robotic swimmer is constructed and both tail shape and propulsive force are measured. Filament

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25

Licata, Julie M. "Physical gesture, spatialization, form and transformation in Watershed I/IV, for solo percussion and real-time computer spatialization, by Roger Reynolds." Thesis, connect to online resource. Recital, recorded Mar. 20, 2006, in digital collections. Access restricted to the University of North Texas campus. Recital, recorded Jan. 29, 2007, in digital collections. Access restricted to the University of North Texas campus, 2009. http://digital.library.unt.edu/ark:/67531/metadc1477.

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26

Lim, Choon Peng. "Experimental investigation of vortex shedding in high Reynolds number flow over compressor blades in cascade." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03Mar%5FLim.pdf.

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Thesis (M.S. in Aeronautical Engineering)--Naval Postgraduate School, March 2003.<br>Thesis advisor(s): Garth V. Hobson, Raymond P. Shreeve. Includes bibliographical references (p. 81-82). Also available online.

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27

Bosco, Arianna [Verfasser]. "Reynolds stress model for hypersonic flows / Arianna Bosco." Aachen : Hochschulbibliothek der Rheinisch-Westfälischen Technischen Hochschule Aachen, 2011. http://d-nb.info/1014297168/34.

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28

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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29

Bose, Jyoti Sankar. "Modeling turbulence anisotropy using algebraic Reynolds stress models." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 1997. http://www.collectionscanada.ca/obj/s4/f2/dsk2/ftp04/mq22277.pdf.

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30

Hall, Jeremiah. "Low Reynolds number aerodynamics for micro aerial vehicles." Connect to online resource, 2007. http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqdiss&rft_dat=xri:pqdiss:1448684.

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31

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 cyli

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32

Nelson, Joshua T. "Practical modification for low Reynolds number propeller applications." Thesis, Wichita State University, 2009. http://hdl.handle.net/10057/2514.

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Applications for Unmanned Aerial Vehicles (UAV) and, specifically, Micro Aerial Vehicles (MAV) are increasing. As is the case for all aircraft, propulsion plays a significant factor in overall vehicle performance. Most small UAV or MAV propellers are commercial, off-the-shelf products given their availability and low cost. Unfortunately, the off-the-shelf propellers are not tailored to a specific vehicle and/or mission. Only limited technical and performance data is available for the propellers. A number of modifications have been used on larger (manned) aircraft propellers and rotors in the p

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33

Usui, Michiko. "AEROMECHANICS OF LOW REYNOLDS NUMBER INFLATABLE/RIGIDIZABLE WINGS." UKnowledge, 2004. http://uknowledge.uky.edu/gradschool_theses/321.

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Use of an inflatable/rigidizable wing is explored for Mars airplane designs. The BIG BLUE (Baseline Inflatable-wing Glider Balloon Launched Unmanned airplane Experiment) project was developed at the University of Kentucky, with an objective to demonstrate feasibility of this technology with a flight-test of an high-altitude glider with inflatable/rigidizable wings. The focus of this thesis research was to design and analyze the wing for this project. The wings are stowed in the fuselage, inflate during ascent, and rigidize with exposure to UV light. The design of wings was evaluated by using a

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34

Gough, Tim. "Low Reynolds number turbulent boundary layers and wakes." Thesis, University of Surrey, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.360949.

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35

Guneratne, Julie Clare. "High Reynolds number flow in a collapsible channel." Thesis, University of Cambridge, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.340767.

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36

Chan, Brian 1980. "Propulsion devices for locomotion at low-Reynolds number." Thesis, Massachusetts Institute of Technology, 2004. http://hdl.handle.net/1721.1/27065.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2004.<br>Includes bibliographical references (leaves 65-66).<br>We have designed, built, and tested three novel devices that use low-Reynolds number flows for self propulsion. The three-link swimmer is designed to swim through in a free viscous fluid using cyclic flipping motion of two rigid fins attached to a rigid midsection. Robosnail 1 uses lubrication pressures underneath a flexible, sinusoidally waving boundary to generate thrust, and Robosnail 2 uses five independently controlled translating feet segm

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37

Shaffer, Damon M. "Reynolds stress measurements downstream of a turbine cascade." Thesis, Virginia Tech, 1985. http://hdl.handle.net/10919/45735.

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An experimental investigation was performed to measure Reynolds stresses in the turbulent flow downstream of a large-scale linear turbine cascade. A rotatable X-wire hot-wire probe that allows redundant data to be taken with solution for mean velocities and turbulence quantities by least-squares fitting procedures was developed. This measurement technique was verified in a fully-developed turbulent pipe flow; the results show the accuracy of the probe when used in an end-flow orientation at various incidence angles and with a multiple number of angular settings. Traverses with a single hot-wi

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38

Staaby, Kirsten. "Postmodern spirituality in the works of Reynolds Price /." Lynchburg, VA : Liberty University, 2007. http://digitalcommons.liberty.edu.

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39

Hamel, Joshua M. "Hydrofoil static pressure acquisition at high Reynolds number." Thesis, Springfield, Va. : Available from National Technical Information Service, 2001. http://handle.dtic.mil/100.2/ADA403412.

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40

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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41

Connelly, Jonathan S. "Streamwise fluctuations of vortex breakdown at high Reynolds numbers." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://library.nps.navy.mil/uhtbin/hyperion/06Jun%5FConnelly.pdf.

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42

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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43

Childs, Laura Helen. "Low Reynolds number flows of generalized non-Newtonian fluids." Thesis, University of Bristol, 2013. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.633090.

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A Newtonian fluid is one for which the stress induced by flow is proportional to the strain rate, with the constant of proportionality being the fluid's viscosity. Fluids not adhering to this linear relationship are described as non-Newtonian. This thesis considers several problems involving flows of generalized non-Newtonian fluids - where the effective viscosity is a nonlinear function of the strain rate - experiencing negligible inertial effects. First, we consider the flow of a power-law fluid through a rectangular duct. We propose a numerical method of solution, reliant on expressing the

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44

Howell, R. J. "Wake-separation bubble interactions in low Reynolds number turbomachinery." Thesis, University of Cambridge, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.604667.

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There is a continual demand for a reduction in the cost and weight of aero-engines. Suppliers of engines always need to reduce manufacturing costs and airlines want to carry more passengers or cargo. This thesis will show that reducing the number of blades in the low pressure turbine is a potent way of achieving both of these goals. Through a program of experimental and numerical work, it is shown how it is possible to reduce the number of blades in the turbine by approximately 15% relative to the first generation of high lift blading employed in the BMW Rolls-Royce BR715 low pressure turbine.

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Davenport, W. J. "Separation bubbles at high Reynolds number : measurement and computation." Thesis, University of Cambridge, 1985. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.232788.

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46

Jones, Anya Rachel. "Unsteady low Reynolds number aerodynamics of a waving wing." Thesis, University of Cambridge, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.608953.

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47

Kirby, Simon. "High Reynolds number flow : past configurations of multiple blades." Thesis, University of East Anglia, 2010. https://ueaeprints.uea.ac.uk/19105/.

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48

Curtis, Mark Peter. "Aspects of low Reynolds number microswimming using singularity methods." Thesis, University of Oxford, 2013. http://ora.ox.ac.uk/objects/uuid:13dcb39b-f5b7-4d46-92d4-21a9afbecd08.

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Three different models, relating to the study of microswimmers immersed in a low Reynolds number ﬂuid, are presented. The underlying, mathematical concepts employed in each are developed using singularity methods of Stokes ﬂow. The ﬁrst topic concerns the motility of an artiﬁcial, three-sphere microswimmer with prescribed, non-reciprocal, internal forces. The swimmer progresses through a low Reynolds number, nonlinear, viscoelastic medium. The model developed illustrates that the presence of the viscoelastic rheology, when compared to a Newtonian environment, increases both the net displacemen

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49

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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50

YODER, DENNIS ALLEN. "ALGEBRAIC REYNOLDS STRESS MODELING OF PLANAR MIXING LAYER FLOWS." University of Cincinnati / OhioLINK, 2005. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1115637717.

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