Chapter 7. Principles of Unsteady - State and Convective Mass Transfer

Similar documents
Daniel López Gaxiola 1 Student View Jason M. Keith

DIFFERENTIAL EQUATIONS

THE BICYCLE RACE ALBERT SCHUELLER

Step 1: Draw a diagram to represent the system. Draw a T-s process diagram to better visualize the processes occurring during the cycle.

3.185 Problem Set 6. Radiation, Intro to Fluid Flow. Solutions

CIRCLE YOUR DIVISION: Div. 1 (9:30 am) Div. 2 (11:30 am) Div. 3 (2:30 pm) Prof. Ruan Prof. Naik Mr. Singh

Q.1. x A =0.8, ε A =δ A *y A = 0.8*5=4 (because feed contains 80 mol% A, y A = 0.8, δ A =((6-1)/1)=5) k= 0.3 hr -1. So, θ = hr Q.

Moisture transport in concrete during wetting/drying cycles

Lecture 2 Phys 798S Spring 2016 Steven Anlage. The heart and soul of superconductivity is the Meissner Effect. This feature uniquely distinguishes

TKP4105 Separation Technology Exercise 1 Mass Transfer Solution to problems

4 Conservation of Momentum

4.5 Evaporation and Diffusion Evaporation and Diffusion through Quiescent Air (page 286) bulk motion of air and j. y a,2, y j,2 or P a,2, P j,2

Correction for Simple System Example and Notes on Laplace Transforms / Deviation Variables ECHE 550 Fall 2002

ME 375 FINAL EXAM Wednesday, May 6, 2009

Section J8b: FET Low Frequency Response

S E V E N. Steady-State Errors SOLUTIONS TO CASE STUDIES CHALLENGES

Conduction Heat transfer: Unsteady state

Study of a Freely Falling Ellipse with a Variety of Aspect Ratios and Initial Angles

A Single Particle Thermal Model for Lithium Ion Batteries

Tables of data and equations are on the last pages of the exam.

The Extended Balanced Truncation Algorithm

Related Rates section 3.9

Radiation Heat Transfer

PHYSICS 211 MIDTERM II 12 May 2004

An Exact Solution for the Deflection of a Clamped Rectangular Plate under Uniform Load

SIMON FRASER UNIVERSITY School of Engineering Science ENSC 320 Electric Circuits II. R 4 := 100 kohm

Lecture 17: Frequency Response of Amplifiers

Practice Problems Solutions. 1. Frame the Problem - Sketch and label a diagram of the motion. Use the equation for acceleration.

POSTER PRESENTATION OF A PAPER BY: Alex Shved, Mark Logillo, Spencer Studley AAPT MEETING, JANUARY, 2002, PHILADELPHIA

Physics 20 Lesson 28 Simple Harmonic Motion Dynamics & Energy

Introduction to Laplace Transform Techniques in Circuit Analysis

Answer keys. EAS 1600 Lab 1 (Clicker) Math and Science Tune-up. Note: Students can receive partial credit for the graphs/dimensional analysis.

s s 1 s = m s 2 = 0; Δt = 1.75s; a =? mi hr

SOLUTIONS FOR TUTORIAL QUESTIONS COURSE TEP Ideal motor speed = 1450rev/min x 12/120 = 145 rev/min

AMS 212B Perturbation Methods Lecture 20 Part 1 Copyright by Hongyun Wang, UCSC. is the kinematic viscosity and ˆp = p ρ 0

Calculation of the temperature of boundary layer beside wall with time-dependent heat transfer coefficient

Topic 7 Fuzzy expert systems: Fuzzy inference

Conservation of Energy

Modeling of Transport and Reaction in a Catalytic Bed Using a Catalyst Particle Model.

1 year n0tes chemistry new st CHAPTER 7 THERMOCHEMISTRY MCQs Q.1 Which of the following statements is contrary to the first law of thermodynamics?

Part I: Multiple-Choice

ME 375 EXAM #1 Tuesday February 21, 2006

CHAPTER 13 FILTERS AND TUNED AMPLIFIERS

Module 4: Time Response of discrete time systems Lecture Note 1

Physics 6A. Practice Midterm #2 solutions. Prepared by Vince Zaccone For Campus Learning Assistance Services at UCSB

Chemistry I Unit 3 Review Guide: Energy and Electrons

Physics Sp Exam #4 Name:

KNOWN: Air undergoes a polytropic process in a piston-cylinder assembly. The work is known.

( 7) ( 9) ( 8) Applying Thermo: an Example of Kinetics - Diffusion. Applying Thermo: an Example of Kinetics - Diffusion. dw = F dr = dr (6) r

Soil Inertia and Shallow Basement Envelope Impact on Cellar Internal Temperature

Lecture 4. Chapter 11 Nise. Controller Design via Frequency Response. G. Hovland 2004

Physics 6A. Practice Midterm #2 solutions

Fundamental Physics of Force and Energy/Work:

PRESSURE WORK EFFECTS IN UNSTEADY CONVECTIVELY DRIVEN FLOW ALONG A VERTICAL PLATE

ENGINEERING OF NUCLEAR REACTORS

MODERN CONTROL SYSTEMS

Ch. 6 Single Variable Control ES159/259

ME 375 FINAL EXAM SOLUTIONS Friday December 17, 2004

Singular perturbation theory

Faculty of Environmental Sciences, Institute of Waste Management and Contaminated Site Treatment. The Simulation Software.

General Considerations Miller Effect Association of Poles with Nodes Common Source Stage Source Follower Differential Pair

Solving Radical Equations

Scale Efficiency in DEA and DEA-R with Weight Restrictions

All Division 01 students, START HERE. All Division 02 students skip the first 10 questions, begin on # (D)

Investigation of application of extractive distillation method in chloroform manufacture

Solving Differential Equations by the Laplace Transform and by Numerical Methods

Practice Midterm #1 Solutions. Physics 6A

On the Use of High-Order Moment Matching to Approximate the Generalized-K Distribution by a Gamma Distribution

R L R L L sl C L 1 sc

Types of Heat Transfer

two equations that govern the motion of the fluid through some medium, like a pipe. These two equations are the

Chapter 1 Basic Description of Laser Diode Dynamics by Spatially Averaged Rate Equations: Conditions of Validity

The Four Kinetic Regimes of Adsorption from Micellar Surfactant Solutions

An Analytical Solution of the Radiative Transfer Equation for Inhomogeneous Finite Medium with Fresnel Boundary Conditions

ELEC NCERT. 1. Which cell will measure standard electrode potential of copper electrode? (g,0.1 bar) H + (aq.,1 M) Cu 2+ (aq.

Modeling in the Frequency Domain

Homework #6. 1. Continuum wave equation. Show that for long wavelengths the equation of motion,, reduces to the continuum elastic wave equation dt

EE 4443/5329. LAB 3: Control of Industrial Systems. Simulation and Hardware Control (PID Design) The Inverted Pendulum. (ECP Systems-Model: 505)

This appendix derives Equations (16) and (17) from Equations (12) and (13).

Practice Problem Solutions. Identify the Goal The acceleration of the object Variables and Constants Known Implied Unknown m = 4.

CHAPTER 8 OBSERVER BASED REDUCED ORDER CONTROLLER DESIGN FOR LARGE SCALE LINEAR DISCRETE-TIME CONTROL SYSTEMS

Online supplementary information

into a discrete time function. Recall that the table of Laplace/z-transforms is constructed by (i) selecting to get

Chapter 7. Root Locus Analysis

Control Systems Engineering ( Chapter 7. Steady-State Errors ) Prof. Kwang-Chun Ho Tel: Fax:

S_LOOP: SINGLE-LOOP FEEDBACK CONTROL SYSTEM ANALYSIS

Application of Newton s Laws. F fr

Jump condition at the boundary between a porous catalyst and a homogeneous fluid

Fair Game Review. Chapter 7 A B C D E Name Date. Complete the number sentence with <, >, or =

Types of Heat Transfer

CONTROL SYSTEMS. Chapter 2 : Block Diagram & Signal Flow Graphs GATE Objective & Numerical Type Questions

Quick Visit to Bernoulli Land

Moment of Inertia of an Equilateral Triangle with Pivot at one Vertex

Finite Element Truss Problem

NONISOTHERMAL OPERATION OF IDEAL REACTORS Plug Flow Reactor

Image Denoising Based on Non-Local Low-Rank Dictionary Learning

AP Physics Momentum AP Wrapup

On the Isentropic Forchheimer s Sound Waves Propagation in a Cylindrical Tube Filled with a Porous Media

Mass Transfer (Stoffaustausch) Fall Semester 2014

ADAPTIVE CONTROL DESIGN FOR A SYNCHRONOUS GENERATOR

Transcription:

Suppleental Material for Tranport Proce and Separation Proce Principle hapter 7 Principle of Unteady - State and onvective Ma Tranfer Thi chapter cover different ituation where a tranfer i taking place, when the condition are changing with tie and where there i a fluid trea that contribute to thee a tranfer procee. The following exaple illutrate convective and tranient a tranfer in fuel cell yte. 7.5- Diffuion and heical Reaction in the node haber of a Direct Methanol Fuel ell 7.5-4 Diffuion of O and O through tagnant itrogen in a Solid Oxide Fuel ell Daniel López Gaxiola 1 Student View Jaon M. Keith

Principle of Unteady State and onvective Ma Tranfer Exaple 7.5- Diffuion and heical Reaction in the node haber of a Direct Methanol Fuel ell n aqueou 40 ole % ethanol olution i entering the anode of a direct ethanol fuel cell. The fuel i diffuing through the ga diffuion layer (GDL) with a thickne of 0.018 c [1]. The diffuion coefficient of the fuel in the GDL i etiated by García et al. [1] to be 1 10. The governing equation for ethanol in the GDL i given by: 9 d dz = 0 with the following boundary condition: t z = 0 : = b t z = δ : = k 1 The rate contant for the cheical reaction occurring at the catalyt layer located at z = δ i 6 k =.8 10. Deterine the olar fraction of ethanol at z = δ and teady tate, if the initial 1 ol concentration b of ethanol i 500. Strategy The olar fraction at the catalyt layer can be obtained by olving the governing differential equation. Solution We can tart by olving the given differential equation given in the proble tateent, a hown in the following tep: d dz = 0 = c 1 (1) d = c dz 1 = Daniel López Gaxiola Student View Jaon M. Keith

Suppleental Material for Tranport Proce and Separation Proce Principle 1. García,.L., Sethuraan, V.., Weidner, J.W., White, R.E., Dougal, R., Journal of Fuel ell Science and Technology, 1, 4 48 (004). pplying the firt boundary condition at z = 0, we have: b = c = Subtituting c into Equation yield: = () t z = δ: = () The equation for ethanol flux through the GDL i decribed by Fick Law, given by: d D dz = (4) t z = δ, the olar flux of ethanol i equal to the reaction rate. Therefore: z =δ = (5) Since thi proce i at teady tate, we can equal Equation 4 and 5 to get: d D = (6) dz Fro Equation 1, we have that c 1 =. Subtituting thi into Equation 6 give: D = (7) We can ubtitute Equation into Equation 7 to olve for c 1, a hown in the following tep: 1 1 ( ) Dc = k Dc = k c δ + k 1 1 1 1 b 1 ( ) c = c 1 = (8) Daniel López Gaxiola Student View Jaon M. Keith

Principle of Unteady State and onvective Ma Tranfer ow we can ubtitute thi equation for c 1 into Equation to yield: = + (9) b Equation 9 can be evaluated at the boundary condition for z = δ to obtain the olar fraction at thi point. Hence, = Reducing thi equation and writing in ter of the olar fraction of ethanol, we have: = ( D + ) (10) where i the overall concentration of the fuel entering the fuel cell. The overall concentration can be obtained by dividing the feed concentration of ethanol b by the feed olar fraction of 0.4. Subtituting nueric value into Equation 10 give: ol H OH ol H OH = ol H OH 4 0.4 ( 1.8 10 ) ol + x ol c = 4 + ( 1.8 10 ) x = Daniel López Gaxiola 4 Student View Jaon M. Keith

Suppleental Material for Tranport Proce and Separation Proce Principle Exaple 7.5-4: Diffuion of O and O through tagnant in a Solid Oxide Fuel ell olid - oxide fuel cell operating at a teperature of 9.15 K and a preure of 1.9 at, i producing O fro an electrocheical reaction of O with oxygen fro air. The partial preure of each ga at the ga diffuion layer the bipolar plate channel, located 0.79 away, are given in the following table. Label Ga Partial Preure (at) at Ga Diffuion Layer Partial Preure (at) at ipolar Plate O 0.47 0.01 O 0.1 0.47 1.1 1.4 Deterine the olar flux of O and O in non diffuing. The diffuion coefficient are given below: D = 5.84 10 D = 5.9 10 D = 7.49 10 5 5 5 Where: = O, = O and =. Thee diffuion coefficient were etiated uing Fuller et al. ethod decribed in Section 6.E of Geankopli. The following equation decribe ulticoponent diffuion for two coponent diffuing in tagnant []: P P + = ln D D RT ( z z1 ) P 1. Geankopli,.J., Ma Tranport Phenoena, Holt, Rinehart and Winton Inc., ew York, 197. Daniel López Gaxiola 5 Student View Jaon M. Keith

Principle of Unteady State and onvective Ma Tranfer 1 1 1 1 D D + + D D P P + P 1 1 1 1 DP D D D D + = ln RT( z z1 ) 1 1 1 1 D D + + D D P P 1 + P 1 1 1 1 1 D D D D In thi proble, the flux will be aued poitive fro the bipolar plate to the ga diffuion layer. Strategy We can deterine the fluxe and by iultaneouly olving the equation given in the proble tateent. Solution Firt, we can ubtitute the preure given and the diffuivity coefficient, a well a the operating condition of the fuel cell. Thu, ln L at ( 9.15K )( ) ol K 1.9 at at + = 5 5 at 5.9 10 7.49 10 We can olve thi equation for by following the next tep: 1.9 at at = ln at 1.1 at ( 9.15K )( ) ol K 7.49 10 5 ol = 0.61 (1) So far we have obtained one of the iultaneou equation for the diffuion proce occurring in thi fuel cell. However, in order to olve thi proble, we need a econd equation, obtained fro the equation for +, a hown below: Daniel López Gaxiola 6 Student View Jaon M. Keith

Suppleental Material for Tranport Proce and Separation Proce Principle ( 1.9at) + = at 4 ( 9.15K)( 7.9 10 ) ol K 1 1 1 1 5 5 5.9 10 5.9 10 + + ( at) ( 0.01 at) + ( 1.9 at) 1 1 1 1 5 5 5.84 10 5.84 10 ln 1 1 1 1 5 5 5.84 10 7.49 10 + + ( 0.1 at ) ( at) + ( 1.9 at) 1 1 1 1 5 5 7.49 10 7.49 10 + In thi equation, it can be een that oe ter have the factor expreion can be iplified a follow: in coon. Thu, thi + ( )( 0.47 at ) ( at ) ( )( 1.9 at) ol + + = ln + ( )( at) ( 0.47 at ) + ( )( 1.9 at) We can further iplify thi equation by reoving the olar flow of oxygen in the denoinator a hown in the following tep: ( ) ( ) ol ln + + + = 0.449 + + () ow we can ubtitute Equation 1 into Equation to get: ( + ) + ( ) ( ) ( ) ol 0.61 1.6 0.61 1.6 + ( 0.61 1.6 ) = ln 0.449 + 0.61 1.6 + 0.61 1.6 Siplifying iilar ter and oving all ter to the left ide, we have: + 1.096 + ln = 0 + Daniel López Gaxiola 7 Student View Jaon M. Keith

Principle of Unteady State and onvective Ma Tranfer Thi equation can be olved by trial and error or uing coputer oftware to obtain the olar flow rate of carbon dioxide to be: ol = We can enter thi value into Equation 1 to deterine the flux of oxygen a hown below: ol ol = 0.61 1.6 ol = The following figure illutrate the diffuion proce occurring in the fuel cell cathode. = 0 Ga Diffuion Layer ipolar Plate Daniel López Gaxiola 8 Student View Jaon M. Keith