Importance of Fluids for the Circulation of Blood, Gas Movement, and Gas Exchange
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
Jean-Baptiste Charles Joseph Bélanger (1790-1874), the Backwater Equation and the Bélanger Equation
THE UNIVERSITY OF QUEENSLAND DIVISION OF CIVIL ENGINEERING REPORT CH69/08 JEAN-BAPTISTE CHARLES JOSEPH BÉLANGER (1790-1874), THE BACKWATER EQUATION AND THE BÉLANGER EQUATION AUTHOR: Hubert CHANSON HYDRAULIC MODEL REPORTS This report is published by the Division of Civil Engineering at the University of Queensland. Lists of recently-published titles of this series and of other publications are provided at the end of this report. Requests for copies of any of these documents should be addressed to the Civil Engineering Secretary. The interpretation and opinions expressed herein are solely those of the author(s). Considerable care has been taken to ensure accuracy of the material presented. Nevertheless, responsibility for the use of this material rests with the user. Division of Civil Engineering The University of Queensland Brisbane QLD 4072 AUSTRALIA Telephone: (61 7) 3365 3619 Fax: (61 7) 3365 4599 URL: http://www.eng.uq.edu.au/civil/ First published in 2008 by Division of Civil Engineering The University of Queensland, Brisbane QLD 4072, Australia © Chanson This book is copyright ISBN No. 9781864999211 The University of Queensland, St Lucia QLD JEAN-BAPTISTE CHARLES JOSEPH BÉLANGER (1790-1874), THE BACKWATER EQUATION AND THE BÉLANGER EQUATION by Hubert CHANSON Professor, Division of Civil Engineering, School of Engineering, The University of Queensland, Brisbane QLD 4072, Australia Ph.: (61 7) 3365 3619, Fax: (61 7) 3365 4599, Email: [email protected] Url: http://www.uq.edu.au/~e2hchans/ REPORT No. CH69/08 ISBN 9781864999211 Division of Civil Engineering, The University of Queensland August 2008 Jean-Baptiste BÉLANGER (1790-1874) (Courtesy of the Bibliothèque de l'Ecole Nationale Supérieure des Ponts et Chaussées) Abstract In an open channel, the transition from a high-velocity open channel flow to a fluvial motion is a flow singularity called a hydraulic jump. -
Lecture 18 Ocean General Circulation Modeling
Lecture 18 Ocean General Circulation Modeling 9.1 The equations of motion: Navier-Stokes The governing equations for a real fluid are the Navier-Stokes equations (con servation of linear momentum and mass mass) along with conservation of salt, conservation of heat (the first law of thermodynamics) and an equation of state. However, these equations support fast acoustic modes and involve nonlinearities in many terms that makes solving them both difficult and ex pensive and particularly ill suited for long time scale calculations. Instead we make a series of approximations to simplify the Navier-Stokes equations to yield the “primitive equations” which are the basis of most general circu lations models. In a rotating frame of reference and in the absence of sources and sinks of mass or salt the Navier-Stokes equations are @ �~v + �~v~v + 2�~ �~v + g�kˆ + p = ~ρ (9.1) t r · ^ r r · @ � + �~v = 0 (9.2) t r · @ �S + �S~v = 0 (9.3) t r · 1 @t �ζ + �ζ~v = ω (9.4) r · cpS r · F � = �(ζ; S; p) (9.5) Where � is the fluid density, ~v is the velocity, p is the pressure, S is the salinity and ζ is the potential temperature which add up to seven dependent variables. 115 12.950 Atmospheric and Oceanic Modeling, Spring '04 116 The constants are �~ the rotation vector of the sphere, g the gravitational acceleration and cp the specific heat capacity at constant pressure. ~ρ is the stress tensor and ω are non-advective heat fluxes (such as heat exchange across the sea-surface).F 9.2 Acoustic modes Notice that there is no prognostic equation for pressure, p, but there are two equations for density, �; one prognostic and one diagnostic. -
Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883
Journal of Aviation/Aerospace Education & Research Volume 13 Number 1 JAAER Fall 2003 Article 1 Fall 2003 Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883 Thomas Forenz Follow this and additional works at: https://commons.erau.edu/jaaer Scholarly Commons Citation Forenz, T. (2003). Assessing the Evolution of the Airborne Generation of Thermal Lift in Aerostats 1783 to 1883. Journal of Aviation/Aerospace Education & Research, 13(1). https://doi.org/10.15394/ jaaer.2003.1559 This Article is brought to you for free and open access by the Journals at Scholarly Commons. It has been accepted for inclusion in Journal of Aviation/Aerospace Education & Research by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Forenz: Assessing the Evolution of the Airborne Generation of Thermal Lif Thermal Lift ASSESSING THE EVOLUTION OF THE AIRBORNE GENERATION OF THERMAL LIFT IN AEROSTATS 1783 TO 1883 Thomas Forenz ABSTRACT Lift has been generated thermally in aerostats for 219 years making this the most enduring form of lift generation in lighter-than-air aviation. In the United States over 3000 thermally lifted aerostats, commonly referred to as hot air balloons, were built and flown by an estimated 12,000 licensed balloon pilots in the last decade. The evolution of controlling fire in hot air balloons during the first century of ballooning is the subject of this article. The purpose of this assessment is to separate the development of thermally lifted aerostats from the general history of aerostatics which includes all gas balloons such as hydrogen and helium lifted balloons as well as thermally lifted balloons. -
Vortex Stretching in Incompressible and Compressible Fluids
Vortex stretching in incompressible and compressible fluids Esteban G. Tabak, Fluid Dynamics II, Spring 2002 1 Introduction The primitive form of the incompressible Euler equations is given by du P = ut + u · ∇u = −∇ + gz (1) dt ρ ∇ · u = 0 (2) representing conservation of momentum and mass respectively. Here u is the velocity vector, P the pressure, ρ the constant density, g the acceleration of gravity and z the vertical coordinate. In this form, the physical meaning of the equations is very clear and intuitive. An alternative formulation may be written in terms of the vorticity vector ω = ∇× u , (3) namely dω = ω + u · ∇ω = (ω · ∇)u (4) dt t where u is determined from ω nonlocally, through the solution of the elliptic system given by (2) and (3). A similar formulation applies to smooth isentropic compressible flows, if one replaces the vorticity ω in (4) by ω/ρ. This formulation is very convenient for many theoretical purposes, as well as for better understanding a variety of fluid phenomena. At an intuitive level, it reflects the fact that rotation is a fundamental element of fluid flow, as exem- plified by hurricanes, tornados and the swirling of water near a bathtub sink. Its derivation from the primitive form of the equations, however, often relies on complex vector identities, which render obscure the intuitive meaning of (4). My purpose here is to present a more intuitive derivation, which follows the tra- ditional physical wisdom of looking for integral principles first, and only then deriving their corresponding differential form. The integral principles associ- ated to (4) are conservation of mass, circulation–angular momentum (Kelvin’s theorem) and vortex filaments (Helmholtz’ theorem). -
Studies on Blood Viscosity During Extracorporeal Circulation
Nagoya ]. med. Sci. 31: 25-50, 1967. STUDIES ON BLOOD VISCOSITY DURING EXTRACORPOREAL CIRCULATION HrsASHI NAGASHIMA 1st Department of Surgery, Nagoya University School of Medicine (Director: Prof Yoshio Hashimoto) ABSTRACT Blood viscosity was studied during extracorporeal circulation by means of a cone in cone viscometer. This rotational viscometer provides sixteen kinds of shear rate, ranging from 0.05 to 250.2 sec-1 • Merits and demerits of the equipment were described comparing with the capillary viscometer. In experimental study it was well demonstrated that the whole blood viscosity showed the shear rate dependency at all hematocrit levels. The influence of the temperature change on the whole blood viscosity was clearly seen when hemato· crit was high and shear rate low. The plasma viscosity was 1.8 cp. at 37°C and Newtonianlike behavior was observed at the same temperature. ·In the hypothermic condition plasma showed shear rate dependency. Viscosity of 10% LMWD was over 2.2 fold as high as that of plasma. The increase of COz content resulted in a constant increase in whole blood viscosity and the increased whole blood viscosity after C02 insufflation, rapidly decreased returning to a little higher level than that in untreated group within 3 minutes. Clinical data were obtained from 27 patients who underwent hypothermic hemodilution perfusion. In the cyanotic group, w hole blood was much more viscous than in the non cyanotic. During bypass, hemodilution had greater influence upon whole blood viscosity than hypothermia, but it went inversely upon the plasma viscosity. The whole blood viscosity was more dependent on dilution rate than amount of diluent in mljkg. -
Compressible Flows for Fluidic Control in Microdevices
COMPRESSIBLE FLOWS FOR FLUIDIC CONTROL IN MICRODEVICES by Dustin S. Chang A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy (Chemical Engineering) in The University of Michigan 2010 Doctoral Committee: Professor Mark A. Burns, Chair Professor Robert M. Ziff Associate Professor Luis P. Bernal Associate Professor Michael Mayer © Dustin S. Chang 2010 To my mom and dad, Sweson and Chaohui, and my grandparents, Po-High and Peyuk … Thank you for all your sacrifices. ii ACKNOWLEDGEMENTS To the casual observer, a doctoral thesis may appear to be the product of a single dedicated—albeit misguided—individual after multiple years of toil. Anyone that has survived the experience will most assuredly tell you that he could not have done it without the many people who supported him along the way. Beginning long before graduate school, my family has been a constant source of encouragement, well-meaning criticism, and material support. I am hugely grateful for my aunts and uncles who never failed to go the extra mile in taking care of me, teaching me, and challenging me to improve. Aunt Hsueh-Rong, Aunt Nancy, Aunt Chao-Lin, Uncle Jeff, Aunt Tina, and Uncle Ming ... Thank you for your love. The only people potentially deserving greater appreciation than these are my mother and father and my grandparents. I have no doubt that none of my meager accomplishments would have been possible without your prayers and unconditional support, both moral and financial. I also have no doubt that all of the aforementioned people are infinitely more enamored with the idea of a Ph.D. -
The Influence of Negative Viscosity on Wind-Driven, Barotropic Ocean
916 JOURNAL OF PHYSICAL OCEANOGRAPHY VOLUME 30 The In¯uence of Negative Viscosity on Wind-Driven, Barotropic Ocean Circulation in a Subtropical Basin DEHAI LUO AND YAN LU Department of Atmospheric and Oceanic Sciences, Ocean University of Qingdao, Key Laboratory of Marine Science and Numerical Modeling, State Oceanic Administration, Qingdao, China (Manuscript received 3 April 1998, in ®nal form 12 May 1999) ABSTRACT In this paper, a new barotropic wind-driven circulation model is proposed to explain the enhanced transport of the western boundary current and the establishment of the recirculation gyre. In this model the harmonic Laplacian viscosity including the second-order term (the negative viscosity term) in the Prandtl mixing length theory is regarded as a tentative subgrid-scale parameterization of the boundary layer near the wall. First, for the linear Munk model with weak negative viscosity its analytical solution can be obtained with the help of a perturbation expansion method. It can be shown that the negative viscosity can result in the intensi®cation of the western boundary current. Second, the fully nonlinear model is solved numerically in some parameter space. It is found that for the ®nite Reynolds numbers the negative viscosity can strengthen both the western boundary current and the recirculation gyre in the northwest corner of the basin. The drastic increase of the mean and eddy kinetic energies can be observed in this case. In addition, the analysis of the time-mean potential vorticity indicates that the negative relative vorticity advection, the negative planetary vorticity advection, and the negative viscosity term become rather important in the western boundary layer in the presence of the negative viscosity. -
Circulation, Lecture 4
4. Circulation A key integral conservation property of fluids is the circulation. For convenience, we derive Kelvin’s circulation theorem in an inertial coordinate system and later transform back to Earth coordinates. In inertial coordinates, the vector form of the momentum equation may be written dV = −α∇p − gkˆ + F, (4.1) dt where kˆ is the unit vector in the z direction and F represents the vector frictional acceleration. Now define a material curve that, however, is constrained to lie at all times on a surface along which some state variable, which we shall refer to for now as s,is a constant. (A state variable is a variable that can be expressed as a function of temperature and pressure.) The picture we have in mind is shown in Figure 3.1. 10 The arrows represent the projection of the velocity vector onto the s surface, and the curve is a material curve in the specific sense that each point on the curve moves with the vector velocity, projected onto the s surface, at that point. Now the circulation is defined as C ≡ V · dl, (4.2) where dl is an incremental length along the curve and V is the vector velocity. The integral is a closed integral around the curve. Differentiation of (4.2) with respect to this gives dC dV dl = · dl + V · . (4.3) dt dt dt Since the curve is a material curve, dl = dV, dt so the integrand of the last term in (4.3) can be written as a perfect derivative and so the term itself vanishes. -
4. Circulation and Vorticity This Chapter Is Mainly Concerned With
4. Circulation and vorticity This chapter is mainly concerned with vorticity. This particular flow property is hard to overestimate as an aid to understanding fluid dynamics, essentially because it is difficult to mod- ify. To provide some context, the chapter begins by classifying all different kinds of motion in a two-dimensional velocity field. Equations are then developed for the evolution of vorticity in three dimensions. The prize at the end of the chapter is a fluid property that is related to vorticity but is even more conservative and therefore more powerful as a theoretical tool. 4.1 Two-dimensional flows According to a theorem of Helmholtz, any two-dimensional flowV()x, y can be decom- posed as V= zˆ × ∇ψ+ ∇χ , (4.1) where the “streamfunction”ψ()x, y and “velocity potential”χ()x, y are scalar functions. The first part of the decomposition is non-divergent and the second part is irrotational. If we writeV = uxˆ + v yˆ for the flow in the horizontal plane, then 4.1 says that u = –∂ψ⁄ ∂y + ∂χ ∂⁄ x andv = ∂ψ⁄ ∂x + ∂χ⁄ ∂y . We define the vertical vorticity ζ and the divergence D as follows: ∂v ∂u 2 ζ =zˆ ⋅ ()∇ × V =------ – ------ = ∇ ψ , (4.2) ∂x ∂y ∂u ∂v 2 D =∇ ⋅ V =------ + ----- = ∇ χ . (4.3) ∂x ∂y Determination of the velocity field givenζ and D requires boundary conditions onψ andχ . Contours ofψ are called “streamlines”. The vorticity is proportional to the local angular velocity aboutzˆ . It is known entirely fromψ()x, y or the first term on the rhs of 4.1. -
Pressure and Piezometry (Pressure Measurement)
PRESSURE AND PIEZOMETRY (PRESSURE MEASUREMENT) What is pressure? .......................................................................................................................................... 1 Pressure unit: the pascal ............................................................................................................................ 3 Pressure measurement: piezometry ........................................................................................................... 4 Vacuum ......................................................................................................................................................... 5 Vacuum generation ................................................................................................................................... 6 Hydrostatic pressure ...................................................................................................................................... 8 Atmospheric pressure in meteorology ...................................................................................................... 8 Liquid level measurement ......................................................................................................................... 9 Archimedes' principle. Buoyancy ............................................................................................................. 9 Weighting objects in air and water ..................................................................................................... 10 Siphons ................................................................................................................................................... -
Aerodynamic Analysis of the Undertray of Formula 1
Treball de Fi de Grau Grau en Enginyeria en Tecnologies Industrials Aerodynamic analysis of the undertray of Formula 1 MEMORY Autor: Alberto Gómez Blázquez Director: Enric Trillas Gay Convocatòria: Juny 2016 Escola Tècnica Superior d’Enginyeria Industrial de Barcelona Aerodynamic analysis of the undertray of Formula 1 INDEX SUMMARY ................................................................................................................................... 2 GLOSSARY .................................................................................................................................... 3 1. INTRODUCTION .................................................................................................................... 4 1.1 PROJECT ORIGIN ................................................................................................................................ 4 1.2 PROJECT OBJECTIVES .......................................................................................................................... 4 1.3 SCOPE OF THE PROJECT ....................................................................................................................... 5 2. PREVIOUS HISTORY .............................................................................................................. 6 2.1 SINGLE-SEATER COMPONENTS OF FORMULA 1 ........................................................................................ 6 2.1.1 Front wing [3] ....................................................................................................................... -
FLIGHTS of FANCY the Air, the Peaceful Silence, and the Grandeur of the Aspect
The pleasure is in the birdlike leap into FLIGHTS OF FANCY the air, the peaceful silence, and the grandeur of the aspect. The terror lurks above and below. An uncontrolled as- A history of ballooning cent means frostbite, asphyxia, and death in the deep purple of the strato- By Steven Shapin sphere; an uncontrolled return shatters bones and ruptures organs. We’ve always aspired to up-ness: up Discussed in this essay: is virtuous, good, ennobling. Spirits are lifted; hopes are raised; imagination Falling Upwards: How We Took to the Air, by Richard Holmes. Pantheon. 416 pages. soars; ideas get off the ground; the sky’s $35. pantheonbooks.com. the limit (unless you reach for the stars). To excel is to rise above others. Levity ome years ago, when I lived in as photo op, as advertisement, as inti- is, after all, opposed to gravity, and you SCalifornia, a colleague—a distin- mate romantic gesture. But that’s not don’t want your hopes dashed, your guished silver-haired English how it all started: in its late-eighteenth- dreams deated, or your imagination historian—got a surprise birthday pres- century beginnings, ballooning was a brought down to earth. ent from his wife: a sunset hot-air- Romantic gesture on the grandest of In 1783, the French inventor and balloon trip. “It sets the perfect stage for scales, and it takes one of the great his- scientist Jacques Alexandre Charles your romantic escapade,” the balloon torians and biographers of the Romantic wrote of the ballooning experience as company’s advertising copy reads, rec- era to retrieve what it once signied.