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Дисертації з теми "(e/D); Flow Reynolds number"

Автор: Grafiati

Опубліковано: 3 червня 2025

Оновлено: 31 липня 2025

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1

Trivilos, Epameinondas. "Performance and flow regimes in plane 2-D diffusers with exit channels at low Reynolds numbers." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03sep%5FTrivilos.pdf.

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Thesis (Mechanical Engineer and M.S. in Mechanical Engineering)--Naval Postgraduate School, September 2003.<br>Thesis advisor(s): Knox T. Millsaps. Includes bibliographical references (p. 79-80). Also available online.

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2

König, Franziska [Verfasser], and Christoph [Akademischer Betreuer] Egbers. "Investigation of high Reynolds number pipe flow - CoLaPipe experiments / Franziska König ; Betreuer: Christoph Egbers." Cottbus : BTU Cottbus - Senftenberg, 2015. http://d-nb.info/1114283894/34.

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3

Fleming, Jonathan Lee. "Experimental investigation of the near wall flow structure of a low Reynolds number 3-D turbulent boundary layer." Diss., Virginia Tech, 1996. http://hdl.handle.net/10919/39120.

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Laser Doppler velocimetry (LDV) measurements and hydrogen-bubble flow-visualization techniques were used to examine the near-wall flow structure of 2-D and 3-D turbulent boundary layers (TBLs) over a range of low Reynolds numbers. The goals of this research were (1) an increased understanding of the flow physics in the near wall region of turbulent boundary layers, (2) to observe and quantify differences between 2-D and 3-D TBL flow structures, and (3) to document Reynolds number effects for 3-D TBLs. An ultimate application of this work would be to improve turbulence modeling for 3-D flows.

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4

Gharakhani, Adrin. "A 3-D vortex-boundary element method for the simulation of unsteady, high Reynolds number flows." Thesis, Massachusetts Institute of Technology, 1995. http://hdl.handle.net/1721.1/11255.

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5

Kai, Yun [Verfasser], Ulrich [Akademischer Betreuer] Teubner, and Joachim [Akademischer Betreuer] Peinke. "Micro shock wave: a study of supersonic compressible flow with low Reynolds number by application of ultra short laser pulse and interferometry / Yun Kai ; Ulrich Teubner, Joachim Peinke." Oldenburg : BIS der Universität Oldenburg, 2018. http://d-nb.info/1162620870/34.

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6

Spiller, Martin [Verfasser]. "Physical and Numerical Experiments of Flow and Transport in Heterogeneous Fractured Media : Single Fracture Flow at High Reynolds Numbers, and Reactive Particle Transport / Martin Spiller." Aachen : Shaker, 2005. http://d-nb.info/1186587210/34.

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7

Fassbender, Jens K. [Verfasser]. "Improved robustness for numerical simulation of turbulent flows around civil transport aircraft at flight Reynolds numbers / Institute of Aerodynamics and Flow Technology Braunschweig. Jens K. Fassbender." Köln : DLR, Bibliotheks- und Informationswesen, 2003. http://d-nb.info/971638691/34.

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8

Yuvaraj, Rakesh. "Analyse de la cascade d’ ́energie dans une couche limite turbulente." Electronic Thesis or Diss., Centrale Lille Institut, 2021. http://www.theses.fr/2021CLIL0012.

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Анотація:

Ce travail consiste à étudier la cascade d’ énergie échelle par échelle dans les écoulements turbulents limités par des parois. L’ équation de Karman-Howarth-Monin-Hill (KHMH)est une équation d’ évolution de δu2, qui est directement liée au contenu énergétique dans l’espace des échelles et intègre différents processus associés aux transferts d’énergie dans l’espace physique et l’espace d’échelle (cascade). Le pic de la moyenne spatio-temporelle du terme cascade se met `a l’ échelle avec la micro- échelle de Taylor modifié dans une région éloignée de la paroi. Le terme de dérivée temporelle mod

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9

Vey, Stefan [Verfasser], Christian Oliver [Akademischer Betreuer] Paschereit, David [Akademischer Betreuer] Greenblatt, and Kunihiko [Akademischer Betreuer] Taira. "Low aspect ratio wing flow control at low reynolds numbers / Stefan Vey. Gutachter: Christian Oliver Paschereit ; David Greenblatt ; Kunihiko Taira. Betreuer: Christian Oliver Paschereit." Berlin : Technische Universität Berlin, 2014. http://d-nb.info/1065669720/34.

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10

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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Анотація:

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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11

Srinivasa, Murthy P. "Low Reynolds Number Airfoil Aerodynamics." Thesis, Indian Institute of Science, 2000. http://hdl.handle.net/2005/229.

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Анотація:

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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12

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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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

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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15

Benson, John D. "Transition to a time periodic flow in a through-flow lid-driven cavity." Thesis, Georgia Institute of Technology, 1991. http://hdl.handle.net/1853/18179.

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16

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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17

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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Анотація:

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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18

Tang, Tongdar Danny. "Periodic flow in a bifurcating tube at moderate reynolds number." Diss., Georgia Institute of Technology, 1990. http://hdl.handle.net/1853/17066.

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19

Cutter, Matthew R. "Dispersion in Steady Pipe Flow with Reynolds Number Under 10,000." University of Cincinnati / OhioLINK, 2004. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1093008636.

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20

Sammataro, Michael A. "Performance of a liquid flow ultra-compact heat exchanger." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://library.nps.navy.mil/uhtbin/hyperion/06Jun%5FSammataro.pdf.

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Анотація:

Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, June 2006.<br>Thesis Advisor(s): Ashok Gopinath, Jose Sinibaldi. "June 2006." Includes bibliographical references (p. 45). Also available in print.

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21

Cleaver, David. "Low Reynolds number flow control through small-amplitude high-frequency motion." Thesis, University of Bath, 2011. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.547620.

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Анотація:

There is currently growing interest in the field of Micro Air Vehicles (MAVs). A MAV is characterized by its low Reynolds numbers flight regime which makes lift and thrust creation a significant challenge. One possible solution inspired by nature is flapping flight, but instead of the large-amplitude low-frequency motion suited to the muscular actuators of nature, small-amplitude high-frequency motion may be more suitable for electrical actuators. In this thesis the effect of small-amplitude high-frequency motion is experimentally investigated focusing on three aspects: general performance imp

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22

Power, Gregory D. "A novel approach for analyzing supersonic high reynolds number flows with separation." Diss., Georgia Institute of Technology, 1990. http://hdl.handle.net/1853/13403.

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23

Keiderling, Felix. "Direct noise computation of high Reynolds number subsonic jet flow using LES /." Zürich : ETH, 2008. http://e-collection.ethbib.ethz.ch/show?type=diss&nr=17955.

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24

Shinde, Pradeep R. "Investigation of Low Reynolds Number Flow and Heat Transfer of Louvered Surfaces." FIU Digital Commons, 2016. http://digitalcommons.fiu.edu/etd/3038.

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Анотація:

This study focuses on the investigation of flow behavior at low Reynolds numbers by the experimental and numerical performance testing of micro-channel heat exchangers. An experimental study of the heat transfers and pressure drop of compact heat exchangers with louvered fins and flat tubes was conducted within a low air-side Reynolds number range of 20 < ReLp < 225. Using an existing low-speed wind tunnel, 26 sample heat exchangers of corrugated louver fin type, were tested. New correlations for Colburn j and Fanning friction f factor have been developed in terms of non-dimensional parameters

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25

Reasor, Jr Daniel A. "NUMERICAL SIMULATION OF TWO FLOW CONTROL APPROACHES FOR LOW REYNOLDS NUMBER APPLICATIONS." UKnowledge, 2007. http://uknowledge.uky.edu/gradschool_theses/461.

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Анотація:

Current research in experimental and computational fluid dynamics is focused in the area of flow control. Flow control devices are usually classified as either passive or active. Plasma actuators are active flow control devices that require input from an external power source. Current efforts have modeled the effects of plasma actuators as a body force near the electrode. The research presented herein focuses on modeling the fluid-plasma interaction seen in dielectric barrier discharge plasma actuators as a body force vector in the region above the embedded electrode using computational fluid

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26

Jones, Lloyd Edward. "Numerical studies of the flow around an airfoil at low Reynolds number." Thesis, University of Southampton, 2008. https://eprints.soton.ac.uk/66082/.

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A study of the °ow around airfoils at low-Reynolds numbers has been performed, by a combination of direct numerical simulation (DNS) and linear stability analy- sis. The behaviour of laminar separation bubbles formed on a NACA-0012 airfoil at Rec = 5 £ 104 and incidence 5± is investigated. Initially volume forcing is introduced in order to promote transition to turbulence. After obtaining su±- cient data from this forced case, the explicitly added disturbances are removed and the simulation run further. With no forcing the turbulence is observed to `self-sustain', with increased turbulence int

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27

Awasthi, Manuj. "High Reynolds Number Turbulent Boundary Layer Flow over Small Forward Facing Steps." Thesis, Virginia Tech, 2012. http://hdl.handle.net/10919/33820.

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Measurements were made on three forward steps with step height to boundary layer ratio of approximately 3.8%, 15% and 60% and Reynolds number based on step height ranging from 6640 to 213,000. The measurements included mean wall pressure, single and 2 point wall pressure fluctuations, single and 2 point velocity fluctuations and, oil flow visualization. Pressure fluctuation measurements were made 5 boundary layer thicknesses upstream of step to 22 boundary layer thickness (or 600 step heights for smallest step size) downstream of the step. The results show that the steps remarkably enhance the

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28

Packard, Nathan Owen. "Active Flow Separation Control of a Laminar Airfoil at Low Reynolds Number." The Ohio State University, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=osu1338315982.

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29

Blyth, Mark Gregory. "Steady flow in dividing and merging pipes." Thesis, Imperial College London, 1999. http://hdl.handle.net/10044/1/7633.

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30

Hallenbeck, Kyle J. "Low Reynolds number water flow characteristics through rectangular micro diffusers/nozzles with a primary focus on major/minor pressure loss, static pressure recovery and flow separation." Orlando, Fla. : University of Central Florida, 2008. http://purl.fcla.edu/fcla/etd/CFE0002391.

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31

Blanc, Philippe Francois. "Acoustic influences on flow over an airfoil at low Reynolds numbers." Thesis, Virginia Polytechnic Institute and State University, 1989. http://hdl.handle.net/10919/53203.

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Анотація:

The dependence of an airfoil stall behavior upon the acoustic l environment was experimentally investigated at a Reynolds number of 200,000. The Wortmann FX-63-137-ESM airfoil section was used for the model with an aspect ratio of 4. Some acoustic disturbances could alter the transition process in the shear layer of the separation bubble on the upper surface of the airfoil. These disturbances could delay the deep leading edge stall or hasten stall recovery in some cases. A good agreement was found with the Crabtree criterion to predict the leading edge stall.<br>Master of Science

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32

Gottapu, Manohar. "Two-phase flow: buoyancy driven flow of a partially miscible droplet at low Reynolds number a thesis presented to the faculty of the Graduate School, Tennessee Technological University /." Click to access online, 2009. http://proquest.umi.com/pqdweb?index=0&did=2000384971&SrchMode=1&sid=3&Fmt=6&VInst=PROD&VType=PQD&RQT=309&VName=PQD&TS=1279288319&clientId=28564.

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33

Hickle, Curtis. "Wind Tunnel renovation, flow verification and flapping wing analysis." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2006. http://library.nps.navy.mil/uhtbin/hyperion/06Jun%5FHickle.pdf.

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Анотація:

Thesis (M.S. in Mechanical Engineering)--Naval Postgraduate School, June 2006.<br>Thesis Advisor(s):Dr. Kevin Jones and Dr. Garth Hobson. "June 2006." Includes bibliographical references (p.79-81). Also available in print.

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34

Doty, Mark C. "Laser doppler anemometer measurements of Reynolds stresses in a fully developed pipe flow." Thesis, This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-03302010-020610/.

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35

Ong, Lih-Yenn. "Experimental and numerical studies of S-shaped diffusing ducts." Thesis, Imperial College London, 1997. http://hdl.handle.net/10044/1/8818.

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36

Chen, Suzhen Aerospace &amp Mechanical Engineering Australian Defence Force Academy UNSW. "An improved low-Reynolds-number k-E [ symbol -dissipation rate]." Awarded by:University of New South Wales - Australian Defence Force Academy. School of Aerospace and Mechanical Engineering, 2000. http://handle.unsw.edu.au/1959.4/38651.

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Анотація:

[Formulae and special characters can only be approximated here. Please see the pdf version of the Abstract for an accurate reproduction.] Since the damping functions employed by most of the low-Reynolds-number models are related to the non-dimensional distance y+[ special character ??? near-wall non-dimensional distance in y direction], which is based on local wall shear stress, these models become invalid for separated flows, because the wall shear stress is zero at the reattachment point. In addition, the pressure-velocity correlation term is neglected in most of these models, although this

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37

Kazi, Sheila K. "Numerical study of simulated low Reynolds number axial turbine blades with flow transition." Thesis, Imperial College London, 2007. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.490816.

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Two main sources of high losses in small axial turbines are the tip leakage loss and the Reynolds number related loss. The extents of these losses are directly related to blade geometry. Due to limitation in manufacturing capabilities and the prohibitive cost of precision engineering often the manufactured blade is very different from the design or the ideal blade shape and as a result the component efficiency degrades. Reynolds number effect plays a very important role in the low efficiency of small axial turbines. The effect of low Reynolds number is essentially separation of the flow result

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38

Frucht, Yaacov I. "High Reynolds number incompressible flow simulation about parachute canopies and similar bluff bodies." Thesis, University of Leicester, 1987. http://hdl.handle.net/2381/9152.

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Анотація:

A model for the flow around bluff bodies has been developed. It is applied to an investigation of parachute canopy aerodynamic characteristics. Since the model assumes an axisymmetric incompressible high Reynolds number flow, it is only applicable to the calculation of aerodynamic characteristics at zero angle of attack. The flow is assumed to separate from the canopy at its surface discontinuity, i.e. the canopy hemline. The vorticity created in the boundary layer over the canopy upper surface is carried downstream, forming a free shear layer. In the flow field vorticity is confined to the th

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39

Weldon, Matthew J. (Matthew Jacob). "Experimental studies of shear stress and flow separation in low Reynolds number flows." Thesis, Massachusetts Institute of Technology, 2007. http://hdl.handle.net/1721.1/39892.

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Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2007.<br>Includes bibliographical references (p. 77-78).<br>Presented here is an experimental investigation of the kinematic theory of separation in unsteady two-dimensional flows, and an evaluation of a novel optical shear stress sensor. Fixed separation in the rotor-oscillator flow is studied for steady, periodic, and quasi-periodic fluid motion. Experimental results are directly compared to numerical simulations, which provide the shear-stress and pressure data required for detecting fixed separation in a

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40

Johnson, Tyler Jay. "Drag measurements across patterned surfaces in a low Reynolds number Couette flow facility." Thesis, [Tuscaloosa, Ala. : University of Alabama Libraries], 2009. http://purl.lib.ua.edu/2128.

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41

Lewis, Tanat. "Numerical simulation of buoyancy-induced flow in a sealed rotating cavity." Thesis, University of Bath, 1999. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.285311.

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42

Walton, Andrew Gerard. "Theory and computation of three-dimensional nonlinear effects in pipe flow transition." Thesis, University College London (University of London), 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.321485.

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43

Sund, Stig. "The Effect of Blockage on High Reynolds Number Flow over a semi-circular Obstacle." Thesis, Norwegian University of Science and Technology, Department of Energy and Process Engineering, 2010. http://urn.kb.se/resolve?urn=urn:nbn:no:ntnu:diva-10815.

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<p>In order to map the effects of blockage and aspect ratio, pressure distributions were measured around four different floor-mounted semi-circular cylinders in nominally two-dimensional flow. Diameters ranged from 0.05m to 0.30m for 0.3·10^5<3.5·10^5. No significant blockage effects were found for B=0.05. It was shown that by using the bulk flow velocity as the reference velocity, blockage and aspect ratio effects could be partially counteracted. The use of the bulk flow velocity was identified to be especially efficient in correcting the base pressure coefficient, but led to a larger variati

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44

Hong, Zhao. "Adaptive subgrid scale modelling and multiple mesh simulation of low Reynolds number channel flow." Thesis, University of Surrey, 1994. http://epubs.surrey.ac.uk/843196/.

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The present study is aimed at enhancing the effectiveness of the large eddy simulation (LES) approach to the computation of turbulent flows by these two methods: i) developing a superior subgrid scale (SGS) model and ii) improving the economy of LES. First of all, the various existing SGS models are extensively investigated, and their advangages and disadvantages are addressed to highlight the areas requiring improvements. This study leads to the construction of a modified SGS dynamic model. In addition, a detailed derivation of the second-order velocity structure function SGS model is made, c

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45

Pritchard, David Thomas. "Some problems in two-phase flow : intertidal mudflats and low Reynolds number gravity currents." Thesis, University of Bristol, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.391189.

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46

Almutari, Jaber. "Large-eddy simulation of flow around an airfoil at low Reynolds number near stall." Thesis, University of Southampton, 2011. https://eprints.soton.ac.uk/181533/.

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47

Thake, Michael Patrick Jr. "Investigation of a Laminar Airfoil with Flow Control and the Effect of Reynolds Number." The Ohio State University, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=osu1292962211.

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48

Galbraith, Marshall Chistopher. "Implicit Large Eddy Simulation of Low-Reynolds-Number Transitional Flow Past the SD7003 Airfoil." University of Cincinnati / OhioLINK, 2009. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1242939414.

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49

Rogers, Daniel R. "Design of a Three-Passage Low Reynolds Number Turbine Cascade with Periodic Flow Conditions." Diss., CLICK HERE for online access, 2008. http://contentdm.lib.byu.edu/ETD/image/etd2684.pdf.

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50

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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