Some Thermodynamic Relations at the Critical Point in Liquid-Vapor Systems (Analyticity/Symmetry/Specific Heats/Critical Exponents/Coexistence Curve) 0

Total Page:16

File Type:pdf, Size:1020Kb

Some Thermodynamic Relations at the Critical Point in Liquid-Vapor Systems (Analyticity/Symmetry/Specific Heats/Critical Exponents/Coexistence Curve) 0 Proc. Nat. Acad. Sci. USA Vol. 69, No. 11, pp. 3436-3439, November 1972 Some Thermodynamic Relations at the Critical Point in Liquid-Vapor Systems (analyticity/symmetry/specific heats/critical exponents/coexistence curve) 0. K. RICE AND DO REN CHANG Department of Chemistry, University of North Carolina, Chapel Hill, N.C. 27514 Contributed by 0. K. Rice, September 2Q, 1972 ABSTRACT The relation of the symmetry of the ther- which follows from modynamic functions with respect to the critical density Pc to the analyticity of the chemical potential above the a.01aP)T = (6916PY('aPlbP)T critical temperature is discussed with the aid of thermo- dynamic considerations. Special consideration is- given to =V((P(P/)P= P-'(bP/?P)T [5] the differential coefficients (624/aT2)p and (Z2P/)T2)p. The discussion is extended to the two-phase region, and some of Then the differentiation of Eq. 3 gives the relations between critical exponents are analyzed. A proof is given that the vapor-pressure curve joins smoothly [6(PCv)/-P]T = CV + p(OCV/1p)T = -T(a2M/rT2), [6] with the critical isochore. The behayior of the entropy along the coexistence curve is considered. Finally, an argu- Let us now apply these equations to the case of particle-hole ment is presented that the Griffiths-Liberman inequality symmetry. In this case pCv is symmetric about Pc, the critical 'y' > #(a - 1) is an-equality. density, since Cv is the heat capacity per mol of particles and p is the density of particles. pCv, then, is the heat capacity per THE ONE-PHASE REGION unit volume. pCv is expected to have a ridge of maxima along There has been some discussion recently about the question of P = Pc, so [P(pCv)/Op]T and, hence, (b2u/aT2)' vanish along the analyticity of the chemical potential/h in the neighborhood Pc- of a critical point. It has been stated that above the critical Actually a lattice-gas model is a somewhat awkward con- temperature, Tc, ,u is analytical along the critical isochore of a cept to use for a representation of a real system, especially if simulated liquid-vapor system if there is particle-hole sym- one wishes to discuss the pressure of the real system, al- metry, as in a lattice gas, and such analyticity is assumed in though this can be done (5a). The essential feature of such a Widom's scaling theory (1). On the other hand, certain models system is that pCv has a maximum at p = PC for any tempera- (2, 3) that lack the particle-hole symmetry do not show this ture. We shall describe such a situation as resulting from par- analyticity; this has been the subject of a detailed discussion ticle-hole symmetry, but shall try to represent the pressure by Widom and Stillinger*. This discussion involved statistical more realistically by supposing that the pressure may, at small mechanical treatment of a fairly complex model. p, be represented by a virial equation It seems possible that a discussion based on thermodynamics P = RTp(1 + Bp) might have advantages both in generality and simplicity. It will be the attempt of this paper to supply such a treatment, for which (b2P/bT2)P = O at p = 0 and and also to consider some of its applications. Our treatment dB d will be based principally upon two well-known thermody- ~p = 2pR 2 + T BI namic equations that involve the molal heat capacity at con- aT26p \ dT dT2J stant volume, Cv, namely (4), From Eq. 4, then Cv = -T(62M/?.T2)v + TV(62P/6T2)V [1] = 2R(2 dB + T dd2B\ and 6T2p\)P dT dT2/ (bCv/aV)7 = T(2P/bT2)V [2] At very low densities, ;z = ;LO + RT ln p, where 1AO, the stan- be the value of = Writing the density as the reciprocal of the molal volume, p = dard chemical potential, would iuat p 1, pro- 1/V, we can recast Eq. 1: vided the ideal gas laws held at that density. Thus, at small densities, and by use of Eq. 6 (noting that the specific heat pCv = -Tp(c2/A/8T2)p + T(C2P//T2)p [3] of an ideal gas is independent of density) We differentiate Eq. 3 with respect to p, holding T constant, (b2A/bT2)P = d2/A5/dT2= -CV0T taking note of the fact that Therefore, (a2IA/ T2)p starts out negative at low p, while PC T/26p = c P/aT2ap [4] (b2P/bT2)P obviously starts out as zero. By differentiation of an approximate but general expression (5b) for B, it appears that, while 2dB/dT is positive, Td2B/dT2 is negative and over- * Manuscript submitted to J. Chem. Phys. balances the former, so b3/a/zT2bp is at first negative. Thus 3436 Downloaded by guest on September 25, 2021 Proc. Nat. Acad. Sci. USA 69 (1972) Thermodynamic Relations at the Critical Point 3437 (62iA/6TP), will have the general character depicted in Fig. 1, and use of Eq. 4 will give a curve for (b2p/bT2), such as that shown. The maximum in Cv will occur at p < Pc, where (b2p/bT2)p = 0, from Eq. 2. At p =PC we may write PcCv=T(=PIOTI)pe [7] from which it may be seen that, as Cv approaches infinity when T above the critical point approaches TC, the behavior of (62p/aT2)", parallels that of Cv. As the critical point is approached, the maxima in Fig. 1 become sharper and sharper, assuming that Cv and, hence, (b2A/bT2)) diverge, until at T, the curves have the appearance shown in Fig. 2. Inasmuch as (b2,u/bT2)pc is zero at all temperatures above T, it is clear that A is an analytic function of T for any tem- perature above T, and continuable through T,. On the other FIG. 2. Same as Fig. 1, for T = T,. hand, (8',u/6T')p is obviously not an analytic function of p at T = T., but it might be possible for 1A to be, though with most scaling hypotheses this is not the case at PC. nated by I) and those just inside the two-phase region (desig- It is now fairly easy to see what happens when we do not nated by II), from which relations between the critical expo- have particle-hole symmetry. We may still suppose that pCv nents may be obtained and related to the behavior of the de- has a maximum at some p for temperatures near T,. The line rivatives mentioned. From the relation (8) of these maxima will not, however, coincide with p = p,. Along CV11 - Cvl = - T()P/lbV)T(dV/dT)2 [8] the critical isochore, then, (b2j/bT2) P will not remain con- stant, but will gradually approach the infinite value at T,, so it where (bP/aV)T is evaluated in the one-phase region just out- cannot be said to be an analytic function of T at T,. It ap- side the phase boundary, Widomt obtained the Rushbrook pears, however, that there is no very essential difference be- inequality for the liquid-vapor case. tween the symmetrical and the nonsymmetrical case. It is worth noting that Eq. 8 has exactly the form of Cp - Cv with dV/dT substituted for (bV/16T)p. CvI is just Cv out- THE TWO-PHASE REGION side the coexistence curve and CVr" takes the place of CP. All the thermodynamic equations that are given in the preced- It is of interest, in the magnetic case, where the magnetic field ing section are also applicable to the two-phase region. In the H and the magnetization 111 take the place of - P and V, two-phase region ,, P and their derivatives with respect to T respectively, that the coexistence curve represents an equilib- are independent of p. Thus, as is well known, Cv is linear in V rium between two phases that are identical except for the di- by Eq. 2 and pCv is linear in p by Eq. 6. If there is particle- rection of magnetization, and hence have the same energy. hole symmetry pCv is constant, which makes (621A/bT2)p zero Thus, CII is independent of how the magnetization changes in by Eq. 6, and there seems to be some empirical evidence that any heating process. Indeed, it is the same thing as CH, since H = 0 under the coexistence curve, and in particular it is (a2i/AT2) , remains finite in actual cases (6, 7). If this is so, and if Cv diverges along the critical isochore (62P/bT2)o will di- specific heat along the coexistence curve. Also, dAM/dT along verge in the same way according to Eq. 1. If they refer to the the coexistence curve is (bM/bT)H, since H is constant along conditions inside the two-phase region, such derivatives as the coexistence curve; thus, we see that Eq. 8 is the exact ('2P/6T2)p and (WA'/aT2)p, involving quantities that are con- analogy of the expression for CH - CM that was used in the stant in the two-phase region, can be written as d2P/dT2 and original analysis of this problem for the magnetic case by d2/M/dT2 where the total derivatives indicate changes along Rushbrook. the coexistence or phase-boundary curve separating the one- Inasmuch as (bP/aV)T is never positive, we may infer, as phase from the two-phase region. There are several relations noted by Stephenson (9), that CvI" is never less than CvI between the quantities just inside the one-phase region (desig- (just as Cp is always greater than Cv, and CH than CM).
Recommended publications
  • VISCOSITY of a GAS -Dr S P Singh Department of Chemistry, a N College, Patna
    Lecture Note on VISCOSITY OF A GAS -Dr S P Singh Department of Chemistry, A N College, Patna A sketchy summary of the main points Viscosity of gases, relation between mean free path and coefficient of viscosity, temperature and pressure dependence of viscosity, calculation of collision diameter from the coefficient of viscosity Viscosity is the property of a fluid which implies resistance to flow. Viscosity arises from jump of molecules from one layer to another in case of a gas. There is a transfer of momentum of molecules from faster layer to slower layer or vice-versa. Let us consider a gas having laminar flow over a horizontal surface OX with a velocity smaller than the thermal velocity of the molecule. The velocity of the gaseous layer in contact with the surface is zero which goes on increasing upon increasing the distance from OX towards OY (the direction perpendicular to OX) at a uniform rate . Suppose a layer ‘B’ of the gas is at a certain distance from the fixed surface OX having velocity ‘v’. Two layers ‘A’ and ‘C’ above and below are taken into consideration at a distance ‘l’ (mean free path of the gaseous molecules) so that the molecules moving vertically up and down can’t collide while moving between the two layers. Thus, the velocity of a gas in the layer ‘A’ ---------- (i) = + Likely, the velocity of the gas in the layer ‘C’ ---------- (ii) The gaseous molecules are moving in all directions due= to −thermal velocity; therefore, it may be supposed that of the gaseous molecules are moving along the three Cartesian coordinates each.
    [Show full text]
  • Viscosity of Gases References
    VISCOSITY OF GASES Marcia L. Huber and Allan H. Harvey The following table gives the viscosity of some common gases generally less than 2% . Uncertainties for the viscosities of gases in as a function of temperature . Unless otherwise noted, the viscosity this table are generally less than 3%; uncertainty information on values refer to a pressure of 100 kPa (1 bar) . The notation P = 0 specific fluids can be found in the references . Viscosity is given in indicates that the low-pressure limiting value is given . The dif- units of μPa s; note that 1 μPa s = 10–5 poise . Substances are listed ference between the viscosity at 100 kPa and the limiting value is in the modified Hill order (see Introduction) . Viscosity in μPa s 100 K 200 K 300 K 400 K 500 K 600 K Ref. Air 7 .1 13 .3 18 .5 23 .1 27 .1 30 .8 1 Ar Argon (P = 0) 8 .1 15 .9 22 .7 28 .6 33 .9 38 .8 2, 3*, 4* BF3 Boron trifluoride 12 .3 17 .1 21 .7 26 .1 30 .2 5 ClH Hydrogen chloride 14 .6 19 .7 24 .3 5 F6S Sulfur hexafluoride (P = 0) 15 .3 19 .7 23 .8 27 .6 6 H2 Normal hydrogen (P = 0) 4 .1 6 .8 8 .9 10 .9 12 .8 14 .5 3*, 7 D2 Deuterium (P = 0) 5 .9 9 .6 12 .6 15 .4 17 .9 20 .3 8 H2O Water (P = 0) 9 .8 13 .4 17 .3 21 .4 9 D2O Deuterium oxide (P = 0) 10 .2 13 .7 17 .8 22 .0 10 H2S Hydrogen sulfide 12 .5 16 .9 21 .2 25 .4 11 H3N Ammonia 10 .2 14 .0 17 .9 21 .7 12 He Helium (P = 0) 9 .6 15 .1 19 .9 24 .3 28 .3 32 .2 13 Kr Krypton (P = 0) 17 .4 25 .5 32 .9 39 .6 45 .8 14 NO Nitric oxide 13 .8 19 .2 23 .8 28 .0 31 .9 5 N2 Nitrogen 7 .0 12 .9 17 .9 22 .2 26 .1 29 .6 1, 15* N2O Nitrous
    [Show full text]
  • Specific Latent Heat
    SPECIFIC LATENT HEAT The specific latent heat of a substance tells us how much energy is required to change 1 kg from a solid to a liquid (specific latent heat of fusion) or from a liquid to a gas (specific latent heat of vaporisation). �����푦 (��) 퐸 ����������푐 ������� ℎ���� �� ������� �� = (��⁄��) = 푓 � ����� (��) �����푦 = ����������푐 ������� ℎ���� �� 퐸 = ��푓 × � ������� × ����� ����� 퐸 � = �� 푦 푓 ����� = ����������푐 ������� ℎ���� �� ������� WORKED EXAMPLE QUESTION 398 J of energy is needed to turn 500 g of liquid nitrogen into at gas at-196°C. Calculate the specific latent heat of vaporisation of nitrogen. ANSWER Step 1: Write down what you know, and E = 99500 J what you want to know. m = 500 g = 0.5 kg L = ? v Step 2: Use the triangle to decide how to 퐸 ��푣 = find the answer - the specific latent heat � of vaporisation. 99500 퐽 퐿 = 0.5 �� = 199 000 ��⁄�� Step 3: Use the figures given to work out 푣 the answer. The specific latent heat of vaporisation of nitrogen in 199 000 J/kg (199 kJ/kg) Questions 1. Calculate the specific latent heat of fusion if: a. 28 000 J is supplied to turn 2 kg of solid oxygen into a liquid at -219°C 14 000 J/kg or 14 kJ/kg b. 183 600 J is supplied to turn 3.4 kg of solid sulphur into a liquid at 115°C 54 000 J/kg or 54 kJ/kg c. 6600 J is supplied to turn 600g of solid mercury into a liquid at -39°C 11 000 J/kg or 11 kJ/kg d.
    [Show full text]
  • Chapter 3 3.4-2 the Compressibility Factor Equation of State
    Chapter 3 3.4-2 The Compressibility Factor Equation of State The dimensionless compressibility factor, Z, for a gaseous species is defined as the ratio pv Z = (3.4-1) RT If the gas behaves ideally Z = 1. The extent to which Z differs from 1 is a measure of the extent to which the gas is behaving nonideally. The compressibility can be determined from experimental data where Z is plotted versus a dimensionless reduced pressure pR and reduced temperature TR, defined as pR = p/pc and TR = T/Tc In these expressions, pc and Tc denote the critical pressure and temperature, respectively. A generalized compressibility chart of the form Z = f(pR, TR) is shown in Figure 3.4-1 for 10 different gases. The solid lines represent the best curves fitted to the data. Figure 3.4-1 Generalized compressibility chart for various gases10. It can be seen from Figure 3.4-1 that the value of Z tends to unity for all temperatures as pressure approach zero and Z also approaches unity for all pressure at very high temperature. If the p, v, and T data are available in table format or computer software then you should not use the generalized compressibility chart to evaluate p, v, and T since using Z is just another approximation to the real data. 10 Moran, M. J. and Shapiro H. N., Fundamentals of Engineering Thermodynamics, Wiley, 2008, pg. 112 3-19 Example 3.4-2 ---------------------------------------------------------------------------------- A closed, rigid tank filled with water vapor, initially at 20 MPa, 520oC, is cooled until its temperature reaches 400oC.
    [Show full text]
  • Thermal Properties of Petroleum Products
    UNITED STATES DEPARTMENT OF COMMERCE BUREAU OF STANDARDS THERMAL PROPERTIES OF PETROLEUM PRODUCTS MISCELLANEOUS PUBLICATION OF THE BUREAU OF STANDARDS, No. 97 UNITED STATES DEPARTMENT OF COMMERCE R. P. LAMONT, Secretary BUREAU OF STANDARDS GEORGE K. BURGESS, Director MISCELLANEOUS PUBLICATION No. 97 THERMAL PROPERTIES OF PETROLEUM PRODUCTS NOVEMBER 9, 1929 UNITED STATES GOVERNMENT PRINTING OFFICE WASHINGTON : 1929 F<ir isale by tfttf^uperintendent of Dotmrtients, Washington, D. C. - - - Price IS cants THERMAL PROPERTIES OF PETROLEUM PRODUCTS By C. S. Cragoe ABSTRACT Various thermal properties of petroleum products are given in numerous tables which embody the results of a critical study of the data in the literature, together with unpublished data obtained at the Bureau of Standards. The tables contain what appear to be the most reliable values at present available. The experimental basis for each table, and the agreement of the tabulated values with experimental results, are given. Accompanying each table is a statement regarding the esti- mated accuracy of the data and a practical example of the use of the data. The tables have been prepared in forms convenient for use in engineering. CONTENTS Page I. Introduction 1 II. Fundamental units and constants 2 III. Thermal expansion t 4 1. Thermal expansion of petroleum asphalts and fluxes 6 2. Thermal expansion of volatile petroleum liquids 8 3. Thermal expansion of gasoline-benzol mixtures 10 IV. Heats of combustion : 14 1. Heats of combustion of crude oils, fuel oils, and kerosenes 16 2. Heats of combustion of volatile petroleum products 18 3. Heats of combustion of gasoline-benzol mixtures 20 V.
    [Show full text]
  • Changes in State and Latent Heat
    Physical State/Latent Heat Changes in State and Latent Heat Physical States of Water Latent Heat Physical States of Water The three physical states of matter that we normally encounter are solid, liquid, and gas. Water can exist in all three physical states at ordinary temperatures on the Earth's surface. When water is in the vapor state, as a gas, the water molecules are not bonded to each other. They float around as single molecules. When water is in the liquid state, some of the molecules bond to each other with hydrogen bonds. The bonds break and re-form continually. When water is in the solid state, as ice, the molecules are bonded to each other in a solid crystalline structure. This structure is six- sided, with each molecule of water connected to four others with hydrogen bonds. Because of the way the crystal is arranged, there is actually more empty space between the molecules than there is in liquid water, so ice is less dense. That is why ice floats. Latent Heat Each time water changes physical state, energy is involved. In the vapor state, the water molecules are very energetic. The molecules are not bonded with each other, but move around as single molecules. Water vapor is invisible to us, but we can feel its effect to some extent, and water vapor in the atmosphere is a very important http://daphne.palomar.edu/jthorngren/latent.htm (1 of 4) [4/9/04 5:30:18 PM] Physical State/Latent Heat factor in weather and climate. In the liquid state, the individual molecules have less energy, and some bonds form, break, then re-form.
    [Show full text]
  • Safety Advice. Cryogenic Liquefied Gases
    Safety advice. Cryogenic liquefied gases. Properties Cryogenic Liquefied Gases are also known as Refrigerated Liquefied Gases or Deeply Refrigerated Gases and are commonly called Cryogenic Liquids. Cryogenic Gases are cryogenic liquids that have been vaporised and may still be at a low temperature. Cryogenic liquids are used for their low temperature properties or to allow larger quantities to be stored or transported. They are extremely cold, with boiling points below -150°C (-238°F). Carbon dioxide and Nitrous oxide, which both have higher boiling points, are sometimes included in this category. In the table you may find some data related to the most common Cryogenic Gases. Helium Hydrogen Nitrogen Argon Oxygen LNG Nitrous Carbon Oxide Dioxide Chemical symbol He H2 N2 Ar O2 CH4 N2O CO2 Boiling point at 1013 mbar [°C] -269 -253 -196 -186 -183 -161 -88.5 -78.5** Density of the liquid at 1013 mbar [kg/l] 0.124 0.071 0.808 1.40 1.142 0.42 1.2225 1.1806 3 Density of the gas at 15°C, 1013 mbar [kg/m ] 0.169 0.085 1.18 1.69 1.35 0.68 3.16 1.87 Relative density (air=1) at 15°C, 1013 mbar * 0.14 0.07 0.95 1.38 1.09 0.60 1.40 1.52 Gas quantity vaporized from 1 litre liquid [l] 748 844 691 835 853 630 662 845 Flammability range n.a. 4%–75% n.a. n.a. n.a. 4.4%–15% n.a. n.a. Notes: *All the above gases are heavier than air at their boiling point; **Sublimation point (where it exists as a solid) Linde AG Gases Division, Carl-von-Linde-Strasse 25, 85716 Unterschleissheim, Germany Phone +49.89.31001-0, [email protected], www.linde-gas.com 0113 – SA04 LCS0113 Disclaimer: The Linde Group has no control whatsoever as regards performance or non-performance, misinterpretation, proper or improper use of any information or suggestions contained in this instruction by any person or entity and The Linde Group expressly disclaims any liability in connection thereto.
    [Show full text]
  • The Particle Model of Matter 5.1
    The Particle Model of Matter 5.1 More than 2000 years ago in Greece, a philosopher named Democritus suggested that matter is made up of tiny particles too small to be seen. He thought that if you kept cutting a substance into smaller and smaller pieces, you would eventually come to the smallest possible particles—the building blocks of matter. Many years later, scientists came back to Democritus’ idea and added to it. The theory they developed is called the particle model of matter. LEARNING TIP There are four main ideas in the particle model: Are you able to explain the 1. All matter is made up of tiny particles. particle model of matter in your own words? If not, re-read the main ideas and examine the illustration that goes with each. 2. The particles of matter are always moving. 3. The particles have spaces between them. 4. Adding heat to matter makes the particles move faster. heat Scientists find the particle model useful for two reasons. First, it provides a reasonable explanation for the behaviour of matter. Second, it presents a very important idea—the particles of matter are always moving. Matter that seems perfectly motionless is not motionless at all. The air you breathe, your books, your desk, and even your body all consist of particles that are in constant motion. Thus, the particle model can be used to explain the properties of solids, liquids, and gases. It can also be used to explain what happens in changes of state (Figure 1 on the next page). NEL 5.1 The Particle Model of Matter 117 The particles in a solid are held together strongly.
    [Show full text]
  • Gas–Solid Reactions Are Very Important in Many Chemical
    Quantized Method Solution for Various Fluid-Solid Reaction Models H. Delavari Amrei*, E. Jamshidi, H. Ale Ebrahim Department of Chemical Engineering, Amirkabir University of Technology (Tehran Polytechnic), Petrochemical Center of Excellency, Tehran 15875-4413, Iran. *Corresponding author. Tel.: +98 21 64543177; fax: +98 21 66405847. E-mail address:[email protected] (H. Delavari Amrei) Abstract Fluid–solid reactions exist in many chemical and metallurgical process industries. Several models describe these reactions such as volume reaction model, grain model, random pore model and nucleation model. These models give two nonlinear coupled partial differential equations (CPDE) that must be solved numerically. A new approximate solution technique (quantized method) has been introduced for some of these models in recent years. In this work, the various fluid-solid reaction models with their quantized and numerical solutions have been discussed. Keywords: Fluid-solid reaction, Quantized method, Mathematical models. 1 Contents 1. Introduction......................................................................................................................................... 3 2. Mathematical models of single pellet reaction and their QM solutions ............................................. 5 2.1. Volume reaction model ................................................................................................................ 5 2.2. Grain model ..............................................................................................................................
    [Show full text]
  • Notes for States of Matter/Boiling, Melting and Freezing Points/ and Changes in Matter
    Notes for States of Matter/Boiling, Melting and Freezing Points/ and Changes in Matter Matter can be described as anything that takes up space and has mass. There are three states of matter: solid, liquid, and gas. Solids have a definite shape and volume. The particles are tightly packed and move very slowly. Liquids have a definite volume but take the shape of the container they are in. The particles are farther apart. The particles move and slide past each other. Gases have no volume or shape. The particles move freely and rapidly. The boiling, freezing and melting points are constant for each type of matter. For water, the boiling point is 100°C/ freezing and melting points are 0°C. Adding salt to water decreases the freezing point of water. That is why salt is put on icy roads in the winter or why salt is added to an old-fashioned ice cream maker. Adding salt to water increases the boiling point of water. States of matter can be changed by adding or lessening heat. When a substance is heated, the particles move rapidly. Heated solid turns into liquid and heated liquid turns into gas. Removing heat (cooling) turns gas into liquid and turns liquid into solid. Evaporation happens when a substances is heated. Condensation happens when a substance is cooled. Notes for States of Matter/Boiling, Melting and Freezing Points/ and Changes in Matter Matter can be described as anything that takes up space and has mass. There are three states of matter: solid, liquid, and gas. Solids have a definite shape and volume.
    [Show full text]
  • Use of Equations of State and Equation of State Software Packages
    USE OF EQUATIONS OF STATE AND EQUATION OF STATE SOFTWARE PACKAGES Adam G. Hawley Darin L. George Southwest Research Institute 6220 Culebra Road San Antonio, TX 78238 Introduction Peng-Robinson (PR) Determination of fluid properties and phase The Peng-Robison (PR) EOS (Peng and Robinson, conditions of hydrocarbon mixtures is critical 1976) is referred to as a cubic equation of state, for accurate hydrocarbon measurement, because the basic equations can be rewritten as cubic representative sampling, and overall pipeline polynomials in specific volume. The Peng Robison operation. Fluid properties such as EOS is derived from the basic ideal gas law along with other corrections, to account for the behavior of compressibility and density are critical for flow a “real” gas. The Peng Robison EOS is very measurement and determination of the versatile and can be used to determine properties hydrocarbon due point is important to verify such as density, compressibility, and sound speed. that heavier hydrocarbons will not condense out The Peng Robison EOS can also be used to of a gas mixture in changing process conditions. determine phase boundaries and the phase conditions of hydrocarbon mixtures. In the oil and gas industry, equations of state (EOS) are typically used to determine the Soave-Redlich-Kwong (SRK) properties and the phase conditions of hydrocarbon mixtures. Equations of state are The Soave-Redlich-Kwaon (SRK) EOS (Soave, 1972) is a cubic equation of state, similar to the Peng mathematical correlations that relate properties Robison EOS. The main difference between the of hydrocarbons to pressure, temperature, and SRK and Peng Robison EOS is the different sets of fluid composition.
    [Show full text]
  • Lecture Notes in Physics Introduction to Plasma Physics
    Lecture Notes in Physics Introduction to Plasma Physics Michael Gedalin ii Contents 1 Basic definitions and parameters 1 1.1 What is plasma . 1 1.2 Debye shielding . 2 1.3 Plasma parameter . 4 1.4 Plasma oscillations . 5 1.5 ∗Ionization degree∗ ............................ 5 1.6 Summary . 6 1.7 Problems . 7 2 Plasma description 9 2.1 Hierarchy of descriptions . 9 2.2 Fluid description . 10 2.3 Continuity equation . 10 2.4 Motion (Euler) equation . 11 2.5 State equation . 12 2.6 MHD . 12 2.7 Order-of-magnitude estimates . 14 2.8 Summary . 14 2.9 Problems . 15 3 MHD equilibria and waves 17 3.1 Magnetic field diffusion and dragging . 17 3.2 Equilibrium conditions . 18 3.3 MHD waves . 19 3.4 Alfven and magnetosonic modes . 22 3.5 Wave energy . 23 3.6 Summary . 24 3.7 Problems . 24 iii CONTENTS 4 MHD discontinuities 27 4.1 Stationary structures . 27 4.2 Discontinuities . 28 4.3 Shocks . 29 4.4 Why shocks ? . 31 4.5 Problems . 32 5 Two-fluid description 33 5.1 Basic equations . 33 5.2 Reduction to MHD . 34 5.3 Generalized Ohm’s law . 35 5.4 Problems . 36 6 Waves in dispersive media 37 6.1 Maxwell equations for waves . 37 6.2 Wave amplitude, velocity etc. 38 6.3 Wave energy . 40 6.4 Problems . 44 7 Waves in two-fluid hydrodynamics 47 7.1 Dispersion relation . 47 7.2 Unmagnetized plasma . 49 7.3 Parallel propagation . 49 7.4 Perpendicular propagation . 50 7.5 General properties of the dispersion relation .
    [Show full text]