PROBLEM 14.6 ( )( ) (b) Applying a species balance to a control volume about the hydrogen, dt 6 dt 6RAT dt 6RT dt

Similar documents
Steady-State Molecular Diffusion

Introduction to Mass Transfer

Differential equations of mass transfer

Outline. Definition and mechanism Theory of diffusion Molecular diffusion in gases Molecular diffusion in liquid Mass transfer

Part I.

Generating cloud drops from CCN. Wallace & Hobbs (1977)

Level 7 Post Graduate Diploma in Engineering Heat and mass transfer

EXPERIMENT 1 DETERMINATION OF GAS DIFFUSION COEFFICIENT

ME 354 Tutorial, Week#13 Reacting Mixtures

Convective Mass Transfer

Mass Transfer Operations

BAE 820 Physical Principles of Environmental Systems

Relationship to Thermodynamics. Chapter One Section 1.3

Chemical Reaction between Solids x 2 = Kt

ASSUMPTIONS: (1) Homogeneous medium with constant properties, (2) Negligible radiation effects.

Find: a) Mass of the air, in kg, b) final temperature of the air, in K, and c) amount of entropy produced, in kj/k.

Fuel, Air, and Combustion Thermodynamics

Transport processes. 7. Semester Chemical Engineering Civil Engineering

Chapter 3 PROPERTIES OF PURE SUBSTANCES. Thermodynamics: An Engineering Approach, 6 th Edition Yunus A. Cengel, Michael A. Boles McGraw-Hill, 2008

Chapter 3 PROPERTIES OF PURE SUBSTANCES

Gestão de Sistemas Energéticos 2017/2018

One-Dimensional, Steady-State. State Conduction without Thermal Energy Generation

Figure Q3. Boundary conditions for a tubular reactor.

Gases. T boil, K. 11 gaseous elements. Rare gases. He, Ne, Ar, Kr, Xe, Rn Diatomic gaseous elements H 2, N 2, O 2, F 2, Cl 2

Solution of a System of ODEs with POLYMATH and MATLAB, Boundary Value Iterations with MATLAB

ME 331 Homework Assignment #6

Thermodynamics I Chapter 2 Properties of Pure Substances

7 Simple mixtures. Solutions to exercises. Discussion questions. Numerical exercises

Summary of Gas Laws V T. Boyle s Law (T and n constant) Charles Law (p and n constant) Combined Gas Law (n constant) 1 =

MSE 360 Exam 1 Spring Points Total

Chapter 11 Solution Thermodynamics: Theory

Chemical Equilibrium Basics

ERT 216 HEAT & MASS TRANSFER SEM2, 2013/2014

Pure Substance. Properties of Pure Substances & Equations of State. Vapour-Liquid-Solid Phase Equilibrium

Using first law of thermodynamics for a constant pressure system: Using first law of thermodynamics for a constant volume system:

MAE 320 THERODYNAMICS FINAL EXAM - Practice. Name: You are allowed three sheets of notes.

By ablation we mean the recession of a surface due to heating, usually by a hot gas. It is the key process for

1.3 Molecular Level Presentation

PROPERTIES OF PURE SUBSTANCES. Chapter 3. Mehmet Kanoglu. Thermodynamics: An Engineering Approach, 6 th Edition. Yunus A. Cengel, Michael A.

ASSUMPTIONS: (1) One-dimensional, radial conduction, (2) Constant properties.

Chemical Thermodynamics : Georg Duesberg

Combustion MATHEMATICAL MODEL FOR TRANSIENT. S. M. Frolov Λ,F.S.Frolov Λ, and B. Basara y

convection coefficient, h c = 18.1 W m K and the surrounding temperature to be 20 C.) (20 marks) Question 3 [35 marks]

CHEM* Physical Chemistry FALL Assignment #1: SOLUTIONS. Gases. Thermodynamics: heat and work

Introduction to Heat and Mass Transfer. Week 10

PROBLEM ρ v (kg/m 3 ) ANALYSIS: The critical heat flux can be estimated by Eq with C = 0.

Comparison of Solids, Liquids, and Gases

LECTURE 1: Disordered solids: Structure properties

ESO201A: Thermodynamics

Diffusional Growth of Liquid Phase Hydrometeros.

Phase Changes and Latent Heat

Chapter 4. Energy Analysis of Closed Systems

MODULE 2: DIFFUSION LECTURE NO. 2

Convective Heat and Mass Transfer Prof. A.W. Date Department of Mechanical Engineering Indian Institute of Technology, Bombay

Chapter 3 PROPERTIES OF PURE SUBSTANCES

Chapter 14 Kinetic Theory

Chapter One Reviews of Thermodynamics Update on 2013/9/13

5.5 Transport Effects at the Interface

PROBLEM h fg ρ v ρ l σ 10 3 T sat (kj/kg) (kg/m 3 ) (N/m) (K)

We can see from the gas phase form of the equilibrium constant that pressure of species depend on pressure. For the general gas phase reaction,

Gases. A gas. Difference between gas and vapor: Why Study Gases?

Mass Transfer Operations-I Prof. Bishnupada Mandal Department of Chemical Engineering Indian Institute of Technology, Guwahati

Chapter 2: The Physical Properties of Pure Compounds

Combustion: Flame Theory and Heat Produced. Arthur Anconetani Oscar Castillo Everett Henderson

Dr Ali Jawarneh Department of Mechanical Engineering Hashemite University

ADSORPTION IN MICROPOROUS MATERIALS: ANALYTICAL EQUATIONS FOR TYPE I ISOTHERMS AT HIGH PRESSURE

( ) PROBLEM C 10 C 1 L m 1 50 C m K W. , the inner surface temperature is. 30 W m K

Physics 5D PRACTICE FINAL EXAM Fall 2013

Control of Proton Electrolyte Membrane Fuel Cell Systems. Dr. M. Grujicic Department of Mechanical Engineering

Chapter 10 Gases Characteristics of Gases Elements that exist as gases: Noble gases, O 2, N 2,H 2, F 2 and Cl 2. (For compounds see table 10.

Gas Density. Standard T & P (STP) 10/29/2011. At STP, 1 mol of any ideal gas occupies 22.4 L. T = 273 K (0 o C) P = 1 atm = kpa = 1.

Thermodynamics Introduction and Basic Concepts

Warning!! Chapter 5 Gases. Chapter Objectives. Chapter Objectives. Chapter Objectives. Air Pollution

Midterm II. ChE 142 April 11, (Closed Book and notes, two 8.5 x11 sheet of notes is allowed) Printed Name

Chapter 11 Gases 1 Copyright McGraw-Hill 2009

Although the molar volumes of liquids can be calculated by means of generalized cubic equations of state, the results are often not of high accuracy.

CHAPTER 8 ENTROPY. Blank

ChE 344 Winter 2011 Mid Term Exam I + Solution. Closed Book, Web, and Notes

C ONTENTS CHAPTER TWO HEAT CONDUCTION EQUATION 61 CHAPTER ONE BASICS OF HEAT TRANSFER 1 CHAPTER THREE STEADY HEAT CONDUCTION 127

Chapter 6 Fundamental Concepts of Convection

KNOWN: Pressure, temperature, and velocity of steam entering a 1.6-cm-diameter pipe.

Properties of Gases. 5 important gas properties:

Pure Substance. Properties of Pure Substances & Equations of State. Vapour-Liquid-Solid Phase Equilibrium

EQUILIBRIUM, MASS CONSERVATION, AND KINETICS

Lecture 18 Molecular Motion and Kinetic Energy

TOPIC 2. Topic 2. States of Matter (I) - Gases. 1

ME Thermodynamics I

Greenhouse Steady State Energy Balance Model

ECH 4224L Unit Operations Lab I Thin Film Evaporator. Introduction. Objective

KINETIC THEORY OF GASES

Chapter 5: The First Law of Thermodynamics: Closed Systems

PROBLEM 8.3 ( ) p = kg m 1m s m 1000 m = kg s m = bar < P = N m 0.25 m 4 1m s = 1418 N m s = 1.

Lectures on Applied Reactor Technology and Nuclear Power Safety. Lecture No 6

Pressure Volume Temperature Relationship of Pure Fluids

MAE 110A. Homework 3: Solutions 10/20/2017

CHE-201. I n t r o d u c t i o n t o Chemical E n g i n e e r i n g. I N S T R U CTOR: D r. N a b e e l S a l i m A b o - Ghander.

1. (25 points) C 6 H O 2 6CO 2 + 7H 2 O C 6 H O 2 6CO + 7H 2 O

Module 1: Mole Balances, Conversion & Reactor Sizing (Chapters 1 and 2, Fogler)

Performance Simulation of Passive Direct Methanol Fuel Cell

Theory. Humidity h of an air-vapor mixture is defined as the mass ratio of water vapor and dry air,

Transcription:

PROBLEM 14.6 KNOWN: Pressure and temperature of hydrogen stored in a spherical steel tank of prescribed diameter and thickness. FIND: (a) Initial rate of hydrogen mass loss from the tank, (b) Initial rate of pressure drop in the tank. SCHEMATIC: ASSUMPTIONS: (1) One-dimensional species diffusion in a stationary medium, () Uniform total molar concentration, C, () No chemical reactions. ANALYSIS: (a) From Table 14.1 or CA,o CA,L CA,o NA,r = = Rm,dif 1/4 DAB 1/r 1/r i o ( ) ( π )( ) 4π 0. 10 1 m /s1.5 kmol/m N 1 A,r = = 7.5 10 kmol/s ( 1/0.05 m1/0.05 m) 1 1 na,r ANA,r kg/kmol 7.5 10 = = kmol/s= 14.7 10 kg/s. M (b) Applying a species balance to a control volume about the hydrogen, Hence M& A,st = M& A,out =na,r ( ρ ) π ρ π π d AV D d A D dpa D A dp M& M A A,st = = = = dt 6 dt 6RAT dt 6RT dt ( )( ) dpa 6R T 60.0814 m bar/kmol K 00 K n 1 A,r 14.7 10 kg/s dt = D = π M A π 0.1m kg/kmol ( ) dp A =.50 10 7 bar/s. dt COMMENTS: If the spherical shell is appoximated as a plane wall, N a,x = D AB (C A,o ) πd /L = 7.07 10-1 kmol/s. This result is 4% lower than that associated with the spherical shell calculation.

PROBLEM 14.1 KNOWN: Oxygen pressures on opposite sides of a rubber membrane. FIND: (a) Molar diffusion flux of O, (b) Molar concentrations of O outside the rubber. SCHEMATIC: ASSUMPTIONS: (1) One-dimensional, steady-state conditions, () Stationary medium of uniform total molar concentration, C = C A + C B, () Perfect gas behavior. PROPERTIES: Table A-8, Oxygen-rubber (98 K): D AB = 0.1 10-9 m /s; Table A-10, Oxygenrubber (98 K): S =.1 10 - kmol/m bar. ANALYSIS: (a) For the assumed conditions From Eq. 14., Hence ( ) ( ) dca CA 0 CA L NA,x = J A,x = DAB = D AB. dx L CA( 0) = SpA,1 = 6.4 10 kmol/m CA( L) = SpA, =.1 10 lmol/m. N 9 A,x = 0.1 10 m /s ( ) 6.4 10.1 10 kmol/m 0.0005 m 9 NA,x = 1.1 10 kmol/s m. (b) From the perfect gas law pa,1 bar C A,1 = = = 0.0807 kmol/m RT 0.0814 m bar/kmol K98 K ( ) CA, = 0.5CA,1 = 0.0404 kmol/m. COMMENTS: Recognize that the molar concentrations outside the membrane differ from those within the membrane; that is, C A,1 C A (0) and C A, C A (L).

PROBLEM 14. KNOWN: Column containing liquid phase of water (A) evaporates into the air (B) flowing over the mouth of the column. FIND: Evaporation rate of water (kg/h m ) using the known value of the binary diffusion coefficient for the water vapor - air mixture. SCHEMATIC: ASSUMPTIONS: (1) Steady-state, one-dimensional diffusion in the column, () Constant properties, () Uniform temperature and pressure throughout the column, (4) Water vapor exhibits ideal gas behavior, and (5) Negligible water vapor in the chamber air. PROPERTIES: Table A-6, water (T = 0 K): p sat = 0.105 bar; Table A-8, water vapor-air (0.5 atm, 0 K): Since D AB ~ p -1 T / find D AB = 0 6 10 4 m /. / s 1.00 / 0.5 0 / 98 = 1157. 10 4 m 1 6 1 6 / s ANALYSIS: Equimolar counter diffusion occurs in the vertical column as water vapor, evaporating at the liquid-vapor interface (x = 0), diffuses up the column through air out into the chamber. From Eq. 14.7, the molar flow rate per unit area is C D N = AB ln 1 x A,L A,x L 1 xa,0 where C is the mixture concentration determined from the ideal gas law as p 0.5 atm C = = = 0.00997 kmol/m RuT 8.05 10 m atm/kmol K 0 K where R u = 8.05 10 m atm/kmol K. The mole fractions at x = 0 and x = L are x A,L = 0 (no water vapor in air above column) xa,0 = pa / p= 0105. / 0. 5 = 0. 41 where p A is the saturation pressure for water at T = 0 K. Substituting numerical values 0. 00997 kmol / m 1157. 10 4 m / s 11 06 N A,x = ln 0.150 m 11 0.416 N = A,x. 964 10 6 kmol / m s or, on a mass basis, m A,x = N A,x MA m = A,x 964. 10 6 kmol / m s 600 s / h 18 kg / kmol m A,x = 0. 57 kg / m h

PROBLEM 14. KNOWN: Radius of coal particles burning in oxygen atmosphere of prescribed pressure and temperature. FIND: (a) Radial distributions of O and CO, (b) O molar consumption rate. SCHEMATIC: ASSUMPTIONS: (1) One-dimensional, steady-state conditions, () Uniform total molar concentration, () No homogeneous chemical reactions, (4) Coal is pure carbon, (5) Surface reaction rate is infinite (hence concentration of O at surface, C A, is zero), (6) Constant D AB, (7) Perfect gas behavior. PROPERTIES: Table A-8, CO O ; D AB (7 K) = 0.14 10-4 m /s; D AB (1450 K) = D AB (7 K) (1450/7) / = 1.71 10-4 m /s. ANALYSIS: (a) For the assumed conditions, Eq. 14.5 reduces to d dc r A 0 dr = dr r ( dc A /dr) = C1 or CA = ( C 1/r) + C. From the boundary conditions: CA( ) = C C = C ( ) CA ro = 0 0 = C 1/ro + C C1 = Cr o. Hence, recognizing that C = C A + C B, CA = C C( r o/r) = C1 ( r o/r) CB = C CA = C( r o/r. ) (b) The conditions correspond to equimolar, counter diffusion ( ) NA = N B, with dxa dca Cr N o A,r = N A,r4πr = CDAB4πr = DAB4πr = 4πDABr + 4πD = ABCr o. dr dr r With find p 1atm C= = = 8.405 10 kmol/m R T 8.05 10 m atm/kmol K 1450 K ( ) N 4 A,r = 1.71 10 m /s 4π 8.405 10 kmol/m 10 m 8 NA,r = 1.81 10 kmol/s.

PROBLEM 14.4 KNOWN: Radius of a spherical organism and molar concentration of oxygen at surface. Diffusion and reaction rate coefficients. FIND: (a) Radial distribution of O concentration, (b) Rate of O consumption, (c) Molar concentration at r = 0. SCHEMATIC: ASSUMPTIONS: (1) Steady-state, one-dimensional diffusion, () Stationary medium, () Uniform total molar concentration, (4) Constant properties (k 0, D AB ). ANALYSIS: (a) For the prescribed conditions and assumptions, Eq. (14.40) reduces to DAB d dca r k 0 = 0 r dr dr dca k0 r r = + C1 dr DAB k 0 r C C 1 A = C 6D AB r + With the requirement that C A (r) remain finite at r = 0, C 1 = 0. With C A (r o ) = C A,o k 0r C o = CA,o 6DAB ( )( ) CA = CA,o k 0/6DAB ro r Because C A cannot be less than zero at any location within the organism, the right-hand side of the foregoing equation must always exceed zero, thereby placing limits on the value of C A,o. The smallest possible value of C A,o is determined from the requirement that C A (0) 0, in which case C A,o k0r o /6DAB ( ) (b) Since oxygen consumption occurs at a uniform volumetric rate of k 0, the total respiration rate is R = k 0, or ( ) π o 0 R = 4/ r k Continued..

PROBLEM 14.4 (Cont.) (c) With r = 0, ( ) = CA 0 CA,o k0r o /6DAB C 5 4 4 8 A 0 = 5 10 kmol / m 1. 10 kmol / s m 10 m / 6 10 m / s ( ) ( ) 5 A ( ) C 0 = 10 kmol/m COMMENTS: (1) The minimum value of C A,o for which a physically realistic solution is possible is C 5 A,o = k0 r o /6DAB = 10 kmol/m. () The total respiration rate may also be obtained by applying Fick s law at r = r o, in which case A ( o ) AB ( π o ) A r= r ( )( ) ( ) o AB π o o AB o π o 0 R = N r =+ D 4 r dc /dr = D 4 R k /6D r = 4/ r k. The result agrees with that of part (b).