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Books on the topic 'Flow around circular cylinder'

Author: Grafiati
Published: 4 June 2021
Last updated: 8 February 2022

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1

Flow around circular cylinders: A comprehensive guide through flow phenomena, experiments, applications, mathematical models, and computer simulations. Oxford: Oxford University Press, 1997.

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2

Gordon, David R. Computational unsteady flow dynamics: Oscillating flow about a circular cylinder. Monterey, Calif: Naval Postgraduate School, 1991.

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3

Lotshaw, John E. Numerical analysis of oscillating flow about a circular cylinder. Monterey, Calif: Naval Postgraduate School, 1992.

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4

Denier, James P. The three-dimensional flow past a rapidly rotating circular cylinder. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1993.

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5

Christopoulos, George P. Oscillating-flow wind tunnel studies for a circulation control circular cylinder. Monterey, Calif: Naval Postgraduate School, 1991.

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6

Wang, Chi R. Application of turbulence modeling to predict surface heat transfer in stagnation flow region of circular cylinder. Cleveland, Ohio: Lewis Research Center, 1987.

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7

Chaplin, David. An improved vortex method for modelling the unsteady development of viscous flow past a circular cylinder. Manchester: University of Manchester, 1995.

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8

Isaacs, D. The use of multipoles in slender-body theory to model the flow around bodies of non-circular cross-section. London: HMSO, 1992.

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9

Stocker, Jennifer Rachel. The study of two problems in fluid mechanics using asymptotic and numerical methods: Part 1 Stationary perturbations of Couette-Poiseuille flow, the flow development in long cavities and channels : part 2 Unsteady flow past a circular cylinder in a rotating frame. Manchester: University of Manchester, 1995.

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10

Borri, Claudio, and Claudio Mannini, eds. Aeroelastic Phenomena and Pedestrian-Structure Dynamic Interaction on Non-Conventional Bridges and Footbridges. Florence: Firenze University Press, 2010. http://dx.doi.org/10.36253/978-88-6453-202-8.

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Fluid-structure and pedestrian-structure interaction phenomena are extremely important for non-conventional bridges. The results presented in this volume concern: simplified formulas for flutter assessment; innovative structural solutions to increase the aeroelastic stability of long-span bridges; numerical simulations of the flow around a benchmark rectangular cylinder; examples of designs of large structures assisted by wind-tunnel tests; analytical, computational and experimental investigation of the synchronisation mechanisms between pedestrians and footbridge structures. The present book is addressed to a wide audience including professionals, doctoral students and researchers, aiming to increase their know-how in the field of wind engineering, bluff-body aerodynamics and bridge dynamics.
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11

Zdravkovich, M. M. Flow Around Circular Cylinders Volume 2 Applications. Oxford University Press, USA, 2002.

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12

Yokuda, Satoru. Study of the dynamics of flow around a circular cylinder at subcritical Reynolds numbers. 1988.

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13

Health & Safety Commission. Wave and Current Flows Around Circular Cylinders at Large Scale. Health and Safety Executive (HSE), 1998.

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14

David, Gottlieb, and Langley Research Center, eds. Spectral simulation of unsteady compressible flow past a circular cylinder. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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15

W, Duck Peter, and Langley Research Center, eds. The three-dimensional flow past a rapidly rotating circular cylinder. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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16

The three-dimensional flow past a rapidly rotating circular cylinder. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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17

W, Duck Peter, and Langley Research Center, eds. The three-dimensional flow past a rapidly rotating circular cylinder. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

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18

S, Cox Jared, and Langley Research Center, eds. Computation of sound generated by viscous flow over a circular cylinder. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

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19

Institute for Computer Applications in Science and Engineering., ed. The inviscid axisymmetric stability of the supersonic flow along a circular cylinder. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1989.

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20

S, Langston L., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., and Lewis Research Center, eds. Measurements of a turbulent horseshoe vortex formed around a cylinder. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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21

Bao, Xiu-Luan. Numerical study of a circular cylinder in regular and random oscillatory flow. 1999.

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22

Center, Langley Research, ed. Stability of the flow around a cylinder: The spin-up problem. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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23

United States. National Aeronautics and Space Administration., ed. Correlations of velocity and temperature fluctuations in the stagnation-point flow of circular cylinder in turbulent flow. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

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24

1945-, Burns John A., and Institute for Computer Applications in Science and Engineering., eds. Optimal control of lift/drag ratios on a rotating cylinder. Hampton, Va: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1991.

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25

Control of separated flow past a cylinder using tangential wall jet blowing. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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26

James, VanFossen G., and Lewis Research Center, eds. The influence of jet-grid turbulence on heat transfer from the stagnation region of a cylinder in crossflow. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

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27

Yuh-Roung, Ou, Pearlstein Arne Jacob 1952-, and Langley Research Center, eds. Development of the wake behind a circular cylinder impulsively started into rotatory and rectilinear motion: Intermediate rotation rates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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28

C, Yeh Frederick, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Application of turbulence modeling to predict surface heat transfer in stagnation flow region of circular cylinder. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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29

C, Yeh Frederick, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Application of turbulence modeling to predict surface heat transfer in stagnation flow region of circular cylinder. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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30

Center, Langley Research, ed. Optimal control of unsteady stokes flow around a cylinder and the sensor/actuator placement problem. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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31

Center, Langley Research, ed. Optimal control of unsteady stokes flow around a cylinder and the sensor/actuator placement problem. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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32

Escudier, Marcel. Internal laminar flow. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0016.

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In this chapter it is shown that solutions to the Navier-Stokes equations can be derived for steady, fully developed flow of a constant-viscosity Newtonian fluid through a cylindrical duct. Such a flow is known as a Poiseuille flow. For a pipe of circular cross section, the term Hagen-Poiseuille flow is used. Solutions are also derived for shear-driven flow within the annular space between two concentric cylinders or in the space between two parallel plates when there is relative tangential movement between the wetted surfaces, termed Couette flows. The concepts of wetted perimeter and hydraulic diameter are introduced. It is shown how the viscometer equations result from the concentric-cylinder solutions. The pressure-driven flow of generalised Newtonian fluids is also discussed.
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33

Ruban, Anatoly I. Boundary-Layer Separation. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199681754.003.0003.

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Chapter 2 discusses the experimental observations of the boundary-layer separation in subsonic and supersonic flows that lead to a formulation of the concept of viscous-inviscid interaction. It then turns to the so-called ‘self-induced separation’ of the boundary layer in supersonic flows. This theory is formulated based on the asymptotic analysis of the Navier–Stokes equations at large values of the Reynolds number. As a part of the flow analysis, this chapter also introduces the ‘triple-deck model’. It then shows how this model may be used to describe the classical problem of the boundary-layer separation in an incompressible fluid flow past a circular cylinder.
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34

Ruban, Anatoly I. Introduction. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199681754.003.0001.

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This book investigates high-Reynolds number flows, and analyses flows that can be described in the framework of Prandtl’s 1904 classical boundary-layer theory, including Blasius’s boundary layer on a flat plate, Falkner–Skan solutions for the boundary layer on a wedge surface, and other applications of Prandtl’s theory. It then discusses separated flows, and considers the so-called ‘self-induced separation’ in supersonic flow, and which led to the ‘triple-deck model’. It also presents Sychev’s 1972 theory of the boundary-layer separation in an incompressible fluid flow past a circular cylinder. It discusses the triple-deck flow near the trailing edge of a flat plate, and then considers the incipience of the separation at corner points of the body surface in subsonic and supersonic flows. It covers the Marginal Separation theory—a special version of the triple-deck theory—and describes the formation and bursting of short separation bubbles at the leading edge of a thin aerofoil.
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35

Ruban, Anatoly I. Fluid Dynamics. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780199681754.001.0001.

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This is Part 3 of a book series on fluid dynamics. This is designed to give a comprehensive and coherent description of fluid dynamics, starting with chapters on classical theory suitable for an introductory undergraduate lecture courses, and then progressing through more advanced material up to the level of modern research in the field. This book is devoted to high-Reynolds number flows. It begins by analysing the flows that can be described in the framework of Prandtl’s 1904 classical boundary-layer theory. These analyses include the Blasius boundary layer on a flat plate, the Falkner-Skan solutions for the boundary layer on a wedge surface, and other applications of Prandtl’s theory. It then discusses separated flows, and considers first the so-called ‘self-induced separation’ in supersonic flow that was studied in 1969 by Stewartson and Williams, as well as by Neiland, and led to the ‘triple-deck model’. It also presents Sychev’s 1972 theory of the boundary-layer separation in an incompressible fluid flow past a circular cylinder. It discusses the triple-deck flow near the trailing edge of a flat plate first investigated in 1969 by Stewartson and in 1970 by Messiter. It then considers the incipience of the separation at corner points of the body surface in subsonic and supersonic flows. It concludes by covering the Marginal Separation theory, which represents a special version of the triple-deck theory, and describes the formation and bursting of short separation bubbles at the leading edge of a thin aerofoil.
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