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Books on the topic 'Equations in fluid flow study'

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Published: 4 June 2021

Last updated: 10 February 2022

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1

Tew, Roy C. Study of two-dimensional compressible non-acoustic modeling of stirling machine type components. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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2

Tew, Roy C. Study of two-dimensional compressible non-acoustic modeling of stirling machine type components. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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3

Tew, Roy C. Study of two-dimensional compressible non-acoustic modeling of stirling machine type components. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2001.

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4

Bergeron, Maurice Denis. A study of the fortified Navier-Stokes approach for viscous airfoil computations. [Toronto, Ont.]: Graduate Department of Aerospace Science and Engineering, University of Toronto, 1994.

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5

Yudaev, Vasiliy. Hydraulics. ru: INFRA-M Academic Publishing LLC., 2021. http://dx.doi.org/10.12737/996354.

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The textbook corresponds to the general education programs of the general courses "Hydraulics" and "Fluid Mechanics". The basic physical properties of liquids, gases, and their mixtures, including the quantum nature of viscosity in a liquid, are described; the laws of hydrostatics, their observation in natural phenomena, and their application in engineering are described. The fundamentals of the kinematics and dynamics of an incompressible fluid are given; original examples of the application of the Bernoulli equation are given. The modes of fluid motion are supplemented by the features of the transient flow mode at high local resistances. The basics of flow similarity are shown. Laminar and turbulent modes of motion in pipes are described, and the classification of flows from a creeping current to four types of hypersonic flow around the body is given. The coefficients of nonuniformity of momentum and kinetic energy for several flows of Newtonian and non-Newtonian fluids are calculated. Examples of solving problems of transient flows by hydraulic methods are given. Local hydraulic resistances, their use in measuring equipment and industry, hydraulic shock, polytropic flow of gas in the pipe and its outflow from the tank are considered. The characteristics of different types of pumps, their advantages and disadvantages, and ways of adjustment are described. A brief biography of the scientists mentioned in the textbook is given, and their contribution to the development of the theory of hydroaeromechanics is shown. The four appendices can be used as a reference to the main text, as well as a subject index. Meets the requirements of the federal state educational standards of higher education of the latest generation. For students of higher educational institutions who study full-time, part-time, evening, distance learning forms of technological and mechanical specialties belonging to the group "Food Technology".

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6

McArdle, Jack G. Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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7

McArdle, Jack G. Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.

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8

ISA--The Instrumentation, Systems, and Automation Society., ed. Flow of industrial fluids: Theory and equations. Boca Raton, Fla: CRC Press, 2004.

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9

Sidilkover, D. Factorizable schemes for the equations of fluid flow. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

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10

Joseph, Daniel D. Fluid dynamics of viscoelastic liquids. New York: Springer-Verlag, 1990.

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11

Whalen, Margaret V. Low Reynolds number nozzle flow study. [Washington, DC]: National Aeronautics and Space Administration, 1987.

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12

Institution, Woods Hole Oceanographic. Summer study program in geophysical fluid dynamics: Patterns in fluid flow. Woods Hole, Mass: Woods Hole Oceanographic Institution, 1991.

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13

Florez, W. F. Nonlinear flow using dual reciprocity. Southampton: WIT, 2001.

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14

A, Rhodes James. A study of flow separation in transonic flow using inviscid and viscous CFD schemes. Norfolk, Va: Institute for Computational and Applied Mechanics (ICAM), Old Dominion University, 1988.

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15

Rummens, H. E. C. Experimental study of flow patterns near tube support structures. Chalk River, Ont: Chalk River Laboratories, 1994.

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16

Ramm, Heinrich J. Fluid dynamics for the study of transonic flow. New York: Oxford University Press, 1990.

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17

Hung, Ching-Mao. Computation of Navier-Stokes equations for three-dimensional flow separation. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1989.

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18

Computational modeling for fluid flow and interfacial transport. Amsterdam: Elsevier, 1994.

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19

Shyy, Wei. Computational modeling for fluid flow and interfacial transport. Amsterdam: Elsevier, 1994.

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20

Pelant, Jaroslav. Inverse problem for two-dimensional flow around a profile. Letnany, Czech Republic: Information Centre for Aeronautics, 1998.

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21

Stern, Frederick. Viscous-inviscid interaction with higher-order viscous-flow equations. Iowa City, Iowa: Iowa Institute of Hydraulic Research, The University of Iowa, 1986.

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22

Chaussee, D. S. High speed viscous flow calculations about complex configurations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1986.

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23

Pelant, Jaroslav. Inverse problem for two-dimensional flow through cascades. Letnany, Czech Republic: Information Centre for Aeronautics, 1998.

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24

Pelant, Jaroslav. Boundary value conditions for Euler equations for three-dimensional flow. Letnany, Czech Republic: Information Centre for Aeronautics, 1998.

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25

Pelant, Jaroslav. Numerical solution of flow of ideal fluid through cascade in a plane. Praha, Czechoslovakia: Information Centre for Aeronautics, 1987.

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26

Mehta, Unmeel B. The computation of flow past an oblique wing using the thin-layer Navier-Stokes equations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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27

Harloff, G. J. Navier-Stokes analysis analysis and experimental data comparison of compressible flow in a diffusing S-duct. [Washington, DC: National Aeronautics and Space Administration, 1992.

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28

Harloff, G. J. Navier-Stokes analysis analysis and experimental data comparison of compressible flow in a diffusing S-duct. [Washington, DC: National Aeronautics and Space Administration, 1992.

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29

Chaussee, D. S. High-speed flow calculations past 3-D configurations based on the Reynolds averaged Navier-Stokes equations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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30

Chaussee, D. S. High-speed flow calculations past 3-D configurations based on the Reynolds averaged Navier-Stokes equations. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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31

Chaderjian, Neal M. Navier-Stokes simulation of transonic wing flow fields using a zonal grid approach. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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32

Chaderjian, Neal M. Navier-Stokes simulation of transonic wing flow fields using a zonal grid approach. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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33

Chaderjian, Neal M. Navier-Stokes simulation of transonic wing flow fields using a zonal grid approach. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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34

Chaderjian, Neal M. Navier-Stokes simulation of transonic wing flow fields using a zonal grid approach. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

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35

Kokkonidis, N. Numerical simulation of viscoelastic fluid flow using integral constitutive equations and finite volume methods. Manchseter: UMIST, 1996.

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36

Speziale, Charles G. On the advantages of the vorticity-velocity formulation of the equations of fluid dynamics. Hampton, Va: ICASE, 1986.

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37

Dynamics of viscous compressible fluids. Oxford: Oxford University Press, 2004.

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38

Dalsem, William R. Van. Some experiences with the viscous-inviscid interaction approach. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1987.

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39

Arthur, Rizzi, and Hirschel Ernst-Heinrich, eds. Numerical solutions of the Euler equations for steady flow problems. Braunschweig; Wiesbaden: Vieweg, 1991.

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40

Eberle, Albrecht. Numerical solutions of the Euler equations for steady flow problems. Braunschweig: Vieweg, 1992.

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41

Dannecker, John D. A numerical study of fluid flow around two-dimensional lifting surfaces. Springfield, Va: Available from National Technical Information Service, 1997.

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42

A computational/experimental study of the flow around a body of revolution at angle of attack. [Washington, DC]: National Aeronautics and Space Administration, 1990.

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43

Bodvarsson, Gudrun M. Solutions to some linear evolutionary systems of equations: Study of the double porosity model of fluid flow in fractured rock and its applications. 1990.

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44

Center, Lewis Research, ed. Numerical study of the effects of icing on viscous flow over wings: Final report. Cleveland, OH: The Center, 1994.

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45

David, Degani, Zilliac Gregory G, and Ames Research Center, eds. Analytical study of the origin and behavior of asymmetric vortices. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1990.

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46

Center, Langley Research, ed. Mach 10 computational study of a three-dimensional scramjet inlet flow field. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

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47

M, Sindir Munir, and United States. National Aeronautics and Space Administration., eds. Comparative study of advanced turbulence models for turbomachinery: Contract NAS8-38860, final report. [Washington, DC: National Aeronautics and Space Administration, 1996.

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48

Escudier, Marcel. Basic equations of viscous-fluid flow. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0015.

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In this chapter it is shown that application of the momentum-conservation equation (Newton’s second law of motion) to an infinitesimal cube of fluid leads to Cauchy’s partial differential equations, which govern the flow of any fluid satisfying the continuum hypothesis. Any fluid flow must also satisfy the continuity equation, another partial differential equation, which is derived from the mass-conservation equation. It is shown that distortion of a flowing fluid can be split into elongational distortion and angular distortion or shear strain. For a Newtonian fluid, the normal and shear stresses in Cauchy’s equations are related to the elongational and shear-strain rates through Stokes’ constitutive equations. Substitution of these constitutive equations into Cauchy’s equations leads to the Navier-Stokes equations, which govern steady or unsteady flow of a fluid. A minor modification of the constitutive equations for a Newtonian fluid allows consideration of generalised Newtonian fluids, for which the viscosity depends upon the shear-strain rates. The boundary conditions for the tangential and normal velocity components are discussed briefly.

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49

Isett, Philip. Hölder Continuous Euler Flows in Three Dimensions with Compact Support in Time. Princeton University Press, 2017. http://dx.doi.org/10.23943/princeton/9780691174822.001.0001.

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Motivated by the theory of turbulence in fluids, the physicist and chemist Lars Onsager conjectured in 1949 that weak solutions to the incompressible Euler equations might fail to conserve energy if their spatial regularity was below 1/3-Hölder. This book uses the method of convex integration to achieve the best-known results regarding nonuniqueness of solutions and Onsager's conjecture. Focusing on the intuition behind the method, the ideas introduced now play a pivotal role in the ongoing study of weak solutions to fluid dynamics equations. The construction itself—an intricate algorithm with hidden symmetries—mixes together transport equations, algebra, the method of nonstationary phase, underdetermined partial differential equations (PDEs), and specially designed high-frequency waves built using nonlinear phase functions. The powerful “Main Lemma”—used here to construct nonzero solutions with compact support in time and to prove nonuniqueness of solutions to the initial value problem—has been extended to a broad range of applications that are surveyed in the appendix. Appropriate for students and researchers studying nonlinear PDEs, this book aims to be as robust as possible and pinpoints the main difficulties that presently stand in the way of a full solution to Onsager's conjecture.

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50

Kyle, Anderson W., Mavriplis Dimitri, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils. [Washington, DC: National Aeronautics and Space Administration, 1995.

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